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T-123SI Technical Information Thermodynamic Properties of HCFC-123 (2,2 dichloro-1,1,1-trifluoroethane) The DuPont Oval Logo, The miracles of science™, and Suva ® , are trademarks or registered trademarks of E.I. du Pont de Nemours and Company. DuPont Suva refrigerants DuPont Product Names: DuPont™ Suva 123 Refrigerant

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Page 1: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

T-123�SI

Technical Information

ThermodynamicPropertiesof

HCFC-123(2,2 dichloro-1,1,1-trifluoroethane)

The DuPont Oval Logo, The miracles of science™,and Suva®, are trademarks or registered trademarks ofE.I. du Pont de Nemours and Company.

DuPont� Suva®

refrigerants

DuPont Product Names:DuPont� Suva® 123 Refrigerant

Page 2: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties
Page 3: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

Thermodynamic Properties of HCFC-123 Refrigerant(2,2 dichloro-1,1,1-trifluoroethane)

SI Units

New tables of the thermodynamic properties of HCFC-123have been developed and are presented here. These tablesare based on experimental data from the database at theNational Institute of Standards and Technology (NIST).Equations have been developed, based on the ModifiedBenedict-Webb-Rubin (MBWR) equation of state, whichrepresent the data with accuracy and consistency through-out the entire range of temperature, pressure, and density.

Physical PropertiesChemical Formula CHCl2CF3

Molecular Weight 152.93

Boiling Point atOne Atmosphere 27.85°C (82.0°F)

Critical Temperature 183.68°C (362.63°F)456.83 K (822.30°R)

Critical Pressure 3668.0 kPa (abs) (532.0 psia)

Critical Density 550.0 kg/m3 (34.34 lb/ft3)

Critical Volume 0.00182 m3/kg (0.0291 ft3/lb)

Units and Factorst = temperature in °C

T = temperature in K = °C + 273.15P = pressure in kiloPascals absolute [kPa (abs)]vf = volume of saturated liquid in m3/kgvg = volume of saturated vapor in m3/kgV = volume of superheated vapor in m3/kgdf = 1/vf = density of saturated liquid in kg/m3

dg = 1/vg = density of saturated vapor in kg/m3

hf = enthalpy of saturated liquid in kJ/kghfg = enthalpy of vaporization in kJ/kghg = enthalpy of saturated vapor in kJ/kgH = enthalpy of superheated vapor in kJ/kgsf = entropy of saturated liquid in kJ/(kg) (K)sg = entropy of saturated vapor in kJ/(kg) (K)S = entropy of superheated vapor in kJ/(kg) (K)

Cp = heat capacity at constant pressure in kJ/(kg) (°C)Cv = heat capacity at constant volume in kJ/(kg) (°C)vs = velocity of sound in m/sec

The gas constant, R = 8.314 J/(mole) (K)for HCFC-123, R = 0.0544 kJ/kg • K

One atmosphere = 101.325 kPaReference point for enthalpy and entropy:

hf = 200 kJ/kg at 0°Csf = 1 kJ/kg • K at 0°C

EquationsThe Modified Benedict-Webb-Rubin (MBWR) equation ofstate was used to calculate the tables of thermodynamicproperties. It was chosen as the preferred equation of statebecause it provided the most accurate fit of the thermo-dynamic data over the entire range of temperatures andpressures presented in these tables. The data fit andcalculation of constants for HCFC-123 were performed forDu Pont at the National Institute of Standards and Tech-nology (NIST) under the supervision of Dr. Mark O.McLinden.

The constants were calculated in SI units. For conversionof thermodynamic properties to Engineering (I/P) units,properties must be calculated in SI units and converted toI/P units. Conversion factors are provided for each prop-erty derived from the MBWR equation of state.

1. Equation of State (MBWR)

P = ΣΣΣΣΣ an/Vn + exp (�Vc2/V2) ΣΣΣΣΣ an/V2n�17

where the temperature dependence of the coefficients isgiven by:

a1 = RT

a2 = b1T + b2T0.5 + b3 + b4/T + b5/T2

a3 = b6T + b7 + b8/T + b9/T2

a4 = b10T + b11 + b12/T

a5 = b13

a6 = b14/T + b15/T2

a7 = b16/T

a8 = b17/T + b18/T2

a9 = b19/T2

a10 = b20/T2 + b21/T3

a11 = b22/T2 + b23/T4

a12 = b24/T2 + b25/T3

a13 = b26/T2 + b27/T4

a14 = b28/T2 + b29/T3

a15 = b30/T2 + b31/T3 + b32/T4

where T is in K = °C + 273.15, P is in kPa, V is inm3/mole, and R = 8.314471

15

n=10

9

n=1

1

Page 4: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

MBWR coefficients for HCFC-123:b1 = –1.973 717 9010 E+00b2 = 1.435 122 7567 E+02b3 = –2.970 987 6039 E+03b4 = 4.505 786 7093 E+05b5 = –4.047 216 7920 E+07b6 = 1.019 193 5793 E–01b7 = –1.963 375 2269 E+02b8 = 9.251 220 6444 E+04b9 = –4.007 630 1858 E+07b10 = –2.040 473 0428 E–02b11 = 3.681 964 8916 E+01b12 = –1.144 525 2703 E+04b13 = –5.509 682 7243 E–01b14 = –7.762 295 1034 E+00b15 = 1.217 213 0502 E+05b16 = –8.286 917 1955 E+00b17 = 7.261 925 3573 E–01b18 = –1.436 309 9944 E+03b19 = 6.425 273 9335 E+01b20 = 3.352 484 9016 E+07b21 = –2.068 382 1999 E+09b22 = 1.825 650 3429 E+06b23 = 4.239 144 7763 E+10b24 = 2.603 669 5332 E+04b25 = 1.307 500 3968 E+07b26 = 1.156 889 5787 E+03b27 = –7.417 765 4079 E+06b28 = –2.449 500 4199 E+00b29 = 4.961 207 9844 E+03b30 = 4.045 163 1009 E–03b31 = 1.214 915 4232 E+02b32 = 2.262 478 6818 E+04

Ideal Gas Heat Capacity Equation (at constantpressure):

Cp (J/mole � K) = cp1 + cp2 T + cp3 T2

cp1 = 2.89811 E+01 cp3 = –1.95477 E–01cp2 = 3.04711 E–01 R = 8.314471 J/mole • K

MW = 152.93

Properties calculated in SI units from the equation andconstants listed above can be converted to I/P unitsusing the conversion factors shown below. Please notethat in converting enthalpy and entropy from SI to I/Punits, a change in reference states must be included(from H = 200 and S = 1 at 0°C for SI units to H = 0and S = 0 at –40°C for I/P units). In the conversionequation below, H (ref) and S (ref) are the saturatedliquid enthalpy and entropy at –40°C. For HCFC-123,H (ref) = 167.2 kJ/kg and S (ref) = 0.8705 kJ/kg • K.

P (psia) = P (kPa) • 0.14504T (°F) = (T[°C] • 1.8) + 32D (lb/ft3) = D (kg/m3) • 0.062428V (ft3/lb) = V (m3/kg) • 16.018H (Btu/lb) = [H (kJ/kg) – H (ref)] • 0.43021S (Btu/lb • °R) = [S (kJ/kg • K) – S (ref)] • 0.23901Cp (Btu/lb • °F) = Cp (kJ/kg • K) • 0.23901Cv (Btu/lb • °F) = Cv (kJ/kg • K) • 0.23901vs (ft/sec) = vs (m/sec) • 3.2808

2. Martin-Hou Equation of State (fit from MBWR data)

As previously stated, the thermodynamic propertiespresented in these tables are based on the MBWRequation of state. Coefficients for the Martin-Houequation of state are presented below for the conve-nience of those who may have existing computerprograms based on this equation of state. While not asaccurate as the data from the MBWR equation of state,particularly in the superheated region, data calculatedusing these Martin-Hou coefficients should be suffi-cient for most engineering calculations.

P = RT/(V�b) + ΣΣΣΣΣ (Ai + BiT + Ci exp (�kT/Tc))/(V�b) i

For SI unitsT and Tc are in K = °C + 273.15, V is in m3/kg,and P is in Kpa

R = 0.0544 kJ/kg • K

b, Ai, Bi, Ci, k are constants:

A2 = –1.770068 E–01 A4 = –9.077682 E–07

B2 = 2.384783 E–04 B4 = 1.955524 E–09

C2 = –1.145981 E+03 C4 = –6.012000 E–01

A3 = 5.579420 E–04 A5 = 4.174049 E–10

B3 = –1.030148 E–06 B5 = –1.035972 E–12

C3 = –4.535924 E+00 C5 = 1.110889 E–03

b = 4.628100 E–04 k = 1.750000 E+01

O

5

i=2

2

Page 5: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

3. Vapor Pressurelog10 Psat = A + B/T + C log10 T + D T +

E ([F�T]/T) log10 (F�T)

For SI unitsT is in K = °C + 273.15 and P is in kPa

A, B, C, D, E, F are constants:

A = 1.656333 E+03 D = –8.868380 E–02

B = –2.480583 E+06 E = 4.617861 E+02

C = 1.792522 E+01 F = 1.666667 E+03

For I/P unitsT is in °R = °F + 459.67 and P is in psia

A, B, C, D, E, F are constants:

A = 1.768800 E+03 D = –4.926878 E–02

B = –4.818693 E+06 E = 4.617861 E+02

C = 1.792522 E+01 F = 3.000000 E+03

4. Density of the Saturated Liquiddf = Af + Bf (1�Tr) (1/3) + Cf (1�Tr) (2/3) + Df (1�Tr)

+ Ef (1�Tr) (4/3)

For SI unitsTr = T/Tc, both in K = °C + 273.15 and df isin kg/m3

Af, Bf, Cf, Df, Ef are constants:

Af = 4.643358 E+02 Df = 1.986142 E+03

Bf = 1.625985 E+03 Ef = –7.172430 E+02

Cf = –1.333543 E+03

For I/P unitsTr = T/Tc, both in °R = °F + 459.67 and df is in lb/ft3

Af, Bf, Cf, Df, Ef are constants:

Af = 2.898754 E+01 Df = 1.239908 E+02

Bf = 1.015069 E+02 Ef = –4.477602 E+01

Cf = –8.325036 E+01

For I/P unitsT and Tc are in °R = °F + 459.67, V is in ft3/lb, andP is in psia

R = 0.0702 (psia)(ft3)/lb • °R

b, Ai, Bi, Ci, k are constants:

A2 = –6.587394 E+00 A4 = –8.668417 E–03

B2 = 4.930603 E–03 B4 = 1.037422 E–05

C2 = –4.264823 E+04 C4 = –5.740950 E+03

A3 = 3.326085 E–01 A5 = 6.384736 E–05

B3 = –3.411704 E–04 B5 = –8.803615 E–08

C3 = –2.704021 E+03 C5 = 1.699245 E+02

b = 7.431500 E–03 k = 1.750000 E+01

Ideal Gas Heat Capacity (at constant vapor):Cv = a + bT + cT2 + dT3 + f/T2

For SI unitsCv = kJ/kg • K

T is in K = °C + 273.15

a, b, c, d, f are constants:

a = –5.397695 E+00 d = 4.340077 E–08

b = 3.275570 E–02 f = 6.622145 E+04

c = –6.358090 E–05

For I/P unitsCv = Btu/lb • °R

T is in °R = °F + 459.67

a, b, c, d, f are constants:

a = –1.290080 E+00 d = 1.778641 E–09

b = 4.349333 E–03 f = 5.128047 E+04

c = –4.690185 E–06

o

o

o

3

Page 6: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

–100 0.00 0.0006 1000.0000 1740.8 0.001 –55.4 379.6 324.2 –0.3074 1.8848 –100–99 0.01 0.0006 1000.0000 1738.7 0.001 –43.3 368.0 324.7 –0.2378 1.8752 –99–98 0.01 0.0006 1000.0000 1736.5 0.001 –31.9 357.1 325.2 –0.1725 1.8662 –98–97 0.01 0.0006 1000.0000 1734.4 0.001 –21.1 346.8 325.7 –0.1111 1.8576 –97–96 0.01 0.0006 1000.0000 1732.2 0.001 –10.9 337.1 326.2 –0.0534 1.8495 –96

–95 0.01 0.0006 1000.0000 1730.1 0.001 –1.3 328.0 326.7 0.0009 1.8418 –95–94 0.02 0.0006 500.0000 1727.9 0.002 7.8 319.4 327.2 0.0518 1.8345 –94–93 0.02 0.0006 500.0000 1725.8 0.002 16.5 311.3 327.7 0.0998 1.8275 –93–92 0.02 0.0006 500.0000 1723.7 0.002 24.6 303.6 328.2 0.1449 1.8209 –92–91 0.03 0.0006 333.3333 1721.5 0.003 32.3 296.4 328.7 0.1872 1.8146 –91

–90 0.03 0.0006 333.3333 1719.4 0.003 39.6 289.7 329.2 0.2271 1.8086 –90–89 0.04 0.0006 250.0000 1717.2 0.004 46.5 283.3 329.7 0.2646 1.8029 –89–88 0.04 0.0006 250.0000 1715.1 0.004 53.0 277.3 330.3 0.2999 1.7975 –88–87 0.05 0.0006 200.0000 1713.0 0.005 59.1 271.6 330.8 0.3330 1.7923 –87–86 0.06 0.0006 166.6667 1710.8 0.006 65.0 266.3 331.3 0.3643 1.7873 –86

–85 0.07 0.0006 142.8571 1708.7 0.007 70.5 261.3 331.8 0.3937 1.7826 –85–84 0.08 0.0006 125.0000 1706.6 0.008 75.7 256.6 332.3 0.4213 1.7780 –84–83 0.09 0.0006 111.1111 1704.4 0.009 80.6 252.2 332.8 0.4474 1.7737 –83–82 0.10 0.0006 100.0000 1702.3 0.010 85.3 248.0 333.4 0.4719 1.7695 –82–81 0.11 0.0006 90.9091 1700.2 0.011 89.7 244.1 333.9 0.4950 1.7656 –81

–80 0.13 0.0006 83.3333 1698.0 0.012 93.9 240.5 334.4 0.5168 1.7617 –80–79 0.14 0.0006 71.4286 1695.9 0.014 97.9 237.0 334.9 0.5373 1.7581 –79–78 0.16 0.0006 66.6667 1693.8 0.015 101.7 233.8 335.5 0.5566 1.7546 –78–77 0.18 0.0006 58.8235 1691.7 0.017 105.2 230.7 336.0 0.5749 1.7512 –77–76 0.20 0.0006 52.6316 1689.5 0.019 108.6 227.9 336.5 0.5921 1.7480 –76

–75 0.23 0.0006 47.6190 1687.4 0.021 111.8 225.2 337.0 0.6083 1.7448 –75–74 0.25 0.0006 43.4783 1685.3 0.023 114.9 222.7 337.6 0.6237 1.7418 –74–73 0.28 0.0006 38.4615 1683.2 0.026 117.8 220.3 338.1 0.6382 1.7389 –73–72 0.31 0.0006 35.7143 1681.0 0.028 120.5 218.1 338.6 0.6519 1.7361 –72–71 0.34 0.0006 32.2581 1678.9 0.031 123.1 216.0 339.2 0.6648 1.7335 –71

–70 0.37 0.0006 29.4118 1676.8 0.034 125.6 214.1 339.7 0.6771 1.7309 –70–69 0.41 0.0006 27.0270 1674.7 0.037 128.0 212.2 340.2 0.6887 1.7284 –69–68 0.45 0.0006 25.0000 1672.6 0.040 130.2 210.5 340.8 0.6997 1.7259 –68–67 0.49 0.0006 22.7273 1670.5 0.044 132.4 208.9 341.3 0.7101 1.7236 –67–66 0.54 0.0006 20.8333 1668.3 0.048 134.4 207.4 341.9 0.7200 1.7213 –66

–65 0.59 0.0006 19.2308 1666.2 0.052 136.4 206.0 342.4 0.7294 1.7192 –65–64 0.64 0.0006 17.5439 1664.1 0.057 138.2 204.7 342.9 0.7383 1.7170 –64–63 0.70 0.0006 16.3934 1662.0 0.061 140.0 203.5 343.5 0.7468 1.7150 –63–62 0.76 0.0006 15.1515 1659.9 0.066 141.7 202.3 344.0 0.7549 1.7130 –62–61 0.83 0.0006 13.8889 1657.8 0.072 143.4 201.2 344.6 0.7626 1.7111 –61

–60 0.90 0.0006 12.8205 1655.6 0.078 144.9 200.2 345.1 0.7699 1.7092 –60–59 0.97 0.0006 11.9048 1653.5 0.084 146.4 199.3 345.7 0.7769 1.7074 –59–58 1.05 0.0006 11.1111 1651.4 0.090 147.9 198.4 346.2 0.7837 1.7057 –58–57 1.14 0.0006 10.3093 1649.3 0.097 149.2 197.5 346.8 0.7901 1.7039 –57–56 1.23 0.0006 9.6154 1647.2 0.104 150.6 196.8 347.3 0.7962 1.7023 –56

–55 1.33 0.0006 8.9286 1645.1 0.112 151.9 196.0 347.9 0.8021 1.7007 –55–54 1.43 0.0006 8.2645 1642.9 0.121 153.1 195.3 348.4 0.8078 1.6991 –54–53 1.54 0.0006 7.7519 1640.8 0.129 154.3 194.7 349.0 0.8133 1.6976 –53–52 1.66 0.0006 7.1942 1638.7 0.139 155.5 194.1 349.5 0.8185 1.6961 –52–51 1.79 0.0006 6.7568 1636.6 0.148 156.6 193.5 350.1 0.8236 1.6947 –51

–50 1.92 0.0006 6.2893 1634.5 0.159 157.7 193.0 350.7 0.8285 1.6933 –50–49 2.06 0.0006 5.8824 1632.3 0.170 158.7 192.5 351.2 0.8332 1.6920 –49–48 2.21 0.0006 5.5249 1630.2 0.181 159.8 192.0 351.8 0.8378 1.6907 –48–47 2.37 0.0006 5.1546 1628.1 0.194 160.8 191.6 352.3 0.8423 1.6894 –47–46 2.54 0.0006 4.8544 1626.0 0.206 161.8 191.1 352.9 0.8466 1.6881 –46

–45 2.72 0.0006 4.5455 1623.8 0.220 162.7 190.8 353.5 0.8508 1.6869 –45–44 2.91 0.0006 4.2735 1621.7 0.234 163.7 190.4 354.0 0.8549 1.6857 –44–43 3.11 0.0006 4.0161 1619.6 0.249 164.6 190.0 354.6 0.8590 1.6846 –43–42 3.32 0.0006 3.7736 1617.4 0.265 165.5 189.7 355.2 0.8629 1.6835 –42–41 3.54 0.0006 3.5461 1615.3 0.282 166.4 189.4 355.7 0.8667 1.6824 –41

Table 1HCFC�123 Saturation Properties�Temperature Table

(continued)

LIQUIDvf

VAPORvg

LIQUID1/vf

VAPOR1/vg

LIQUIDhf

LATENThfg

LIQUIDsf

VAPORsg

ENTROPYkJ/(kg)(K)

VAPORhg

PRESSUREkPa (abs)

TEMP.°C

TEMP.°C

VOLUMEm3/kg

DENSITYkg/m3

ENTHALPYkJ/kg

4

Page 7: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

–40 3.78 0.0006 3.3333 1613.1 0.300 167.2 189.1 356.3 0.8705 1.6814 –40–39 4.03 0.0006 3.1447 1611.0 0.318 168.1 188.8 356.9 0.8741 1.6803 –39–38 4.29 0.0006 2.9586 1608.8 0.338 168.9 188.5 357.4 0.8778 1.6793 –38–37 4.57 0.0006 2.7933 1606.7 0.358 169.8 188.2 358.0 0.8813 1.6784 –37–36 4.86 0.0006 2.6316 1604.5 0.380 170.6 188.0 358.6 0.8848 1.6774 –36

–35 5.17 0.0006 2.4876 1602.4 0.402 171.4 187.7 359.2 0.8883 1.6765 –35–34 5.50 0.0006 2.3474 1600.2 0.426 172.3 187.5 359.7 0.8917 1.6756 –34–33 5.84 0.0006 2.2222 1598.0 0.450 173.1 187.2 360.3 0.8951 1.6748 –33–32 6.20 0.0006 2.1008 1595.9 0.476 173.9 187.0 360.9 0.8985 1.6739 –32–31 6.58 0.0006 1.9841 1593.7 0.504 174.7 186.8 361.5 0.9018 1.6731 –31

–30 6.98 0.0006 1.8797 1591.5 0.532 175.5 186.6 362.0 0.9050 1.6723 –30–29 7.40 0.0006 1.7794 1589.3 0.562 176.3 186.3 362.6 0.9083 1.6716 –29–28 7.84 0.0006 1.6863 1587.1 0.593 177.1 186.1 363.2 0.9115 1.6708 –28–27 8.30 0.0006 1.6000 1584.9 0.625 177.9 185.9 363.8 0.9148 1.6701 –27–26 8.78 0.0006 1.5175 1582.7 0.659 178.6 185.7 364.4 0.9180 1.6694 –26

–25 9.29 0.0006 1.4388 1580.5 0.695 179.4 185.5 364.9 0.9211 1.6687 –25–24 9.82 0.0006 1.3661 1578.3 0.732 180.2 185.3 365.5 0.9243 1.6681 –24–23 10.38 0.0006 1.2970 1576.1 0.771 181.0 185.1 366.1 0.9275 1.6674 –23–22 10.96 0.0006 1.2330 1573.9 0.811 181.8 184.9 366.7 0.9306 1.6668 –22–21 11.58 0.0006 1.1723 1571.7 0.853 182.6 184.7 367.3 0.9338 1.6662 –21

–20 12.22 0.0006 1.1148 1569.5 0.897 183.4 184.5 367.9 0.9369 1.6656 –20–19 12.88 0.0006 1.0604 1567.2 0.943 184.2 184.3 368.4 0.9401 1.6651 –19–18 13.58 0.0006 1.0091 1565.0 0.991 185.0 184.1 369.0 0.9432 1.6646 –18–17 14.32 0.0006 0.9615 1562.7 1.040 185.8 183.8 369.6 0.9463 1.6640 –17–16 15.08 0.0006 0.9158 1560.5 1.092 186.6 183.6 370.2 0.9495 1.6636 –16

–15 15.88 0.0006 0.8726 1558.2 1.146 187.4 183.4 370.8 0.9526 1.6631 –15–14 16.71 0.0006 0.8319 1556.0 1.202 188.2 183.2 371.4 0.9557 1.6626 –14–13 17.58 0.0006 0.7937 1553.7 1.260 189.0 183.0 372.0 0.9589 1.6622 –13–12 18.48 0.0006 0.7576 1551.4 1.320 189.8 182.7 372.6 0.9620 1.6618 –12–11 19.43 0.0006 0.7231 1549.2 1.383 190.7 182.5 373.2 0.9651 1.6614 –11

–10 20.41 0.0006 0.6906 1546.9 1.448 191.5 182.3 373.8 0.9683 1.6610 –10–9 21.44 0.0006 0.6596 1544.6 1.516 192.3 182.0 374.4 0.9714 1.6606 –9–8 22.50 0.0006 0.6305 1542.3 1.586 193.2 181.8 375.0 0.9746 1.6603 –8–7 23.61 0.0006 0.6028 1540.0 1.659 194.0 181.6 375.6 0.9777 1.6599 –7–6 24.77 0.0007 0.5764 1537.7 1.735 194.8 181.3 376.2 0.9809 1.6596 –6

–5 25.97 0.0007 0.5516 1535.4 1.813 195.7 181.1 376.7 0.9841 1.6593 –5–4 27.22 0.0007 0.5277 1533.1 1.895 196.5 180.8 377.3 0.9872 1.6590 –4–3 28.52 0.0007 0.5053 1530.8 1.979 197.4 180.6 377.9 0.9904 1.6588 –3–2 29.87 0.0007 0.4840 1528.4 2.066 198.3 180.3 378.5 0.9936 1.6585 –2–1 31.27 0.0007 0.4638 1526.1 2.156 199.1 180.0 379.1 0.9968 1.6583 –1

0 32.73 0.0007 0.4444 1523.7 2.250 200.0 179.7 379.7 1.0000 1.6580 01 34.24 0.0007 0.4263 1521.4 2.346 200.9 179.5 380.3 1.0032 1.6578 12 35.81 0.0007 0.4088 1519.0 2.446 201.8 179.2 380.9 1.0064 1.6577 23 37.43 0.0007 0.3922 1516.7 2.550 202.6 178.9 381.6 1.0096 1.6575 34 39.12 0.0007 0.3764 1514.3 2.657 203.5 178.6 382.2 1.0129 1.6573 4

5 40.86 0.0007 0.3614 1512.0 2.767 204.4 178.3 382.8 1.0161 1.6572 56 42.67 0.0007 0.3471 1509.6 2.881 205.3 178.0 383.4 1.0193 1.6570 67 44.54 0.0007 0.3334 1507.2 2.999 206.3 177.7 384.0 1.0226 1.6569 78 46.48 0.0007 0.3204 1504.8 3.121 207.2 177.4 384.6 1.0258 1.6568 89 48.49 0.0007 0.3081 1502.4 3.246 208.1 177.1 385.2 1.0291 1.6567 9

10 50.57 0.0007 0.2962 1500.0 3.376 209.0 176.8 385.8 1.0323 1.6567 1011 52.72 0.0007 0.2849 1497.6 3.510 209.9 176.5 386.4 1.0356 1.6566 1112 54.94 0.0007 0.2741 1495.2 3.648 210.9 176.1 387.0 1.0389 1.6565 1213 57.23 0.0007 0.2639 1492.7 3.790 211.8 175.8 387.6 1.0421 1.6565 1314 59.61 0.0007 0.2541 1490.3 3.936 212.7 175.5 388.2 1.0454 1.6565 14

15 62.06 0.0007 0.2447 1487.9 4.087 213.7 175.1 388.8 1.0487 1.6565 1516 64.59 0.0007 0.2357 1485.4 4.243 214.6 174.8 389.4 1.0520 1.6565 1617 67.20 0.0007 0.2271 1483.0 4.403 215.6 174.4 390.0 1.0553 1.6565 1718 69.90 0.0007 0.2189 1480.5 4.568 216.6 174.1 390.6 1.0586 1.6565 1819 72.68 0.0007 0.2111 1478.1 4.738 217.5 173.7 391.3 1.0619 1.6566 19

LIQUIDvf

VAPORvg

LIQUID1/vf

VAPOR1/vg

LIQUIDhf

LATENThfg

LIQUIDsf

VAPORsg

ENTROPYkJ/(kg)(K)

VAPORhg

PRESSUREkPa (abs)

TEMP.°C

TEMP.°C

VOLUMEm3/kg

DENSITYkg/m3

ENTHALPYkJ/kg

Table 1 (continued)

HCFC�123 Saturation Properties�Temperature Table

5

Page 8: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

20 75.55 0.0007 0.2035 1475.6 4.913 218.5 173.4 391.9 1.0652 1.6566 2021 78.52 0.0007 0.1963 1473.1 5.093 219.5 173.0 392.5 1.0685 1.6567 2122 81.57 0.0007 0.1895 1470.6 5.278 220.4 172.7 393.1 1.0718 1.6567 2223 84.71 0.0007 0.1828 1468.1 5.469 221.4 172.3 393.7 1.0751 1.6568 2324 87.95 0.0007 0.1766 1465.6 5.664 222.4 171.9 394.3 1.0784 1.6569 24

25 91.29 0.0007 0.1705 1463.1 5.866 223.4 171.5 394.9 1.0817 1.6570 2526 94.73 0.0007 0.1647 1460.6 6.073 224.4 171.1 395.5 1.0850 1.6572 2627 98.27 0.0007 0.1591 1458.1 6.285 225.4 170.8 396.1 1.0884 1.6573 2728 101.92 0.0007 0.1538 1455.6 6.504 226.4 170.4 396.8 1.0917 1.6574 2829 105.66 0.0007 0.1486 1453.0 6.728 227.4 170.0 397.4 1.0950 1.6576 29

30 109.52 0.0007 0.1437 1450.5 6.958 228.4 169.6 398.0 1.0983 1.6577 3031 113.49 0.0007 0.1390 1447.9 7.195 229.4 169.2 398.6 1.1016 1.6579 3132 117.57 0.0007 0.1344 1445.4 7.438 230.4 168.8 399.2 1.1050 1.6581 3233 121.76 0.0007 0.1301 1442.8 7.687 231.4 168.4 399.8 1.1083 1.6583 3334 126.07 0.0007 0.1259 1440.2 7.943 232.5 168.0 400.4 1.1116 1.6585 34

35 130.49 0.0007 0.1219 1437.7 8.205 233.5 167.5 401.0 1.1149 1.6587 3536 135.04 0.0007 0.1180 1435.1 8.474 234.5 167.1 401.6 1.1183 1.6589 3637 139.71 0.0007 0.1143 1432.5 8.750 235.5 166.7 402.3 1.1216 1.6591 3738 144.51 0.0007 0.1107 1429.9 9.033 236.6 166.3 402.9 1.1249 1.6593 3839 149.43 0.0007 0.1073 1427.2 9.323 237.6 165.9 403.5 1.1282 1.6596 39

40 154.48 0.0007 0.1039 1424.6 9.621 238.7 165.4 404.1 1.1316 1.6598 4041 159.66 0.0007 0.1007 1422.0 9.926 239.7 165.0 404.7 1.1349 1.6601 4142 164.98 0.0007 0.0977 1419.3 10.238 240.8 164.6 405.3 1.1382 1.6603 4243 170.43 0.0007 0.0947 1416.7 10.558 241.8 164.1 405.9 1.1415 1.6606 4344 176.03 0.0007 0.0919 1414.0 10.885 242.9 163.7 406.5 1.1448 1.6609 44

45 181.76 0.0007 0.0891 1411.4 11.221 243.9 163.2 407.1 1.1481 1.6612 4546 187.63 0.0007 0.0865 1408.7 11.565 245.0 162.8 407.8 1.1514 1.6615 4647 193.65 0.0007 0.0839 1406.0 11.917 246.0 162.3 408.4 1.1547 1.6618 4748 199.82 0.0007 0.0815 1403.3 12.277 247.1 161.9 409.0 1.1580 1.6621 4849 206.14 0.0007 0.0791 1400.6 12.646 248.2 161.4 409.6 1.1613 1.6624 49

50 212.61 0.0007 0.0768 1397.9 13.023 249.2 161.0 410.2 1.1646 1.6627 5051 219.24 0.0007 0.0746 1395.2 13.410 250.3 160.5 410.8 1.1679 1.6630 5152 226.02 0.0007 0.0724 1392.4 13.805 251.4 160.0 411.4 1.1712 1.6634 5253 232.96 0.0007 0.0704 1389.7 14.209 252.4 159.6 412.0 1.1745 1.6637 5354 240.07 0.0007 0.0684 1386.9 14.623 253.5 159.1 412.6 1.1778 1.6640 54

55 247.33 0.0007 0.0665 1384.2 15.046 254.6 158.6 413.2 1.1811 1.6644 5556 254.77 0.0007 0.0646 1381.4 15.478 255.7 158.1 413.8 1.1843 1.6647 5657 262.38 0.0007 0.0628 1378.6 15.920 256.8 157.6 414.4 1.1876 1.6651 5758 270.15 0.0007 0.0611 1375.8 16.373 257.9 157.2 415.0 1.1909 1.6655 5859 278.10 0.0007 0.0594 1373.0 16.835 258.9 156.7 415.6 1.1941 1.6658 59

60 286.23 0.0007 0.0578 1370.2 17.307 260.0 156.2 416.2 1.1974 1.6662 6061 294.54 0.0007 0.0562 1367.4 17.790 261.1 155.7 416.8 1.2006 1.6666 6162 303.03 0.0007 0.0547 1364.5 18.284 262.2 155.2 417.4 1.2039 1.6669 6263 311.70 0.0007 0.0532 1361.7 18.788 263.3 154.7 418.0 1.2071 1.6673 6364 320.57 0.0007 0.0518 1358.8 19.303 264.4 154.2 418.6 1.2104 1.6677 64

65 329.62 0.0007 0.0504 1356.0 19.830 265.5 153.7 419.2 1.2136 1.6681 6566 338.86 0.0007 0.0491 1353.1 20.368 266.6 153.2 419.8 1.2168 1.6685 6667 348.30 0.0007 0.0478 1350.2 20.917 267.7 152.7 420.4 1.2200 1.6689 6768 357.93 0.0007 0.0466 1347.3 21.478 268.8 152.2 421.0 1.2233 1.6693 6869 367.77 0.0007 0.0453 1344.4 22.051 269.9 151.6 421.6 1.2265 1.6697 69

70 377.81 0.0007 0.0442 1341.4 22.636 271.0 151.1 422.1 1.2297 1.6701 7071 388.05 0.0007 0.0430 1338.5 23.234 272.1 150.6 422.7 1.2329 1.6705 7172 398.50 0.0007 0.0419 1335.5 23.844 273.2 150.1 423.3 1.2361 1.6709 7273 409.17 0.0008 0.0409 1332.6 24.467 274.3 149.6 423.9 1.2393 1.6713 7374 420.04 0.0008 0.0398 1329.6 25.103 275.5 149.0 424.5 1.2424 1.6717 74

75 431.13 0.0008 0.0388 1326.6 25.752 276.6 148.5 425.1 1.2456 1.6721 7576 442.45 0.0008 0.0379 1323.6 26.415 277.7 148.0 425.6 1.2488 1.6726 7677 453.98 0.0008 0.0369 1320.6 27.091 278.8 147.4 426.2 1.2520 1.6730 7778 465.74 0.0008 0.0360 1317.5 27.781 279.9 146.9 426.8 1.2551 1.6734 7879 477.72 0.0008 0.0351 1314.5 28.486 281.0 146.3 427.4 1.2583 1.6738 79

Table 1HCFC�123 Saturation Properties�Temperature Table

(continued)

LIQUIDvf

VAPORvg

LIQUID1/vf

VAPOR1/vg

LIQUIDhf

LATENThfg

LIQUIDsf

VAPORsg

ENTROPYkJ/(kg)(K)

VAPORhg

PRESSUREkPa (abs)

TEMP.°C

TEMP.°C

VOLUMEm3/kg

DENSITYkg/m3

ENTHALPYkJ/kg

6

Page 9: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

80 489.93 0.0008 0.0342 1311.4 29.205 282.2 145.8 427.9 1.2614 1.6742 8081 502.38 0.0008 0.0334 1308.3 29.938 283.3 145.2 428.5 1.2646 1.6746 8182 515.06 0.0008 0.0326 1305.2 30.687 284.4 144.7 429.1 1.2677 1.6751 8283 527.98 0.0008 0.0318 1302.1 31.450 285.5 144.1 429.6 1.2708 1.6755 8384 541.15 0.0008 0.0310 1299.0 32.230 286.6 143.6 430.2 1.2740 1.6759 84

85 554.55 0.0008 0.0303 1295.9 33.025 287.8 143.0 430.8 1.2771 1.6763 8586 568.21 0.0008 0.0296 1292.7 33.836 288.9 142.4 431.3 1.2802 1.6767 8687 582.11 0.0008 0.0288 1289.6 34.663 290.0 141.8 431.9 1.2833 1.6772 8788 596.27 0.0008 0.0282 1286.4 35.507 291.2 141.3 432.4 1.2864 1.6776 8889 610.68 0.0008 0.0275 1283.2 36.368 292.3 140.7 433.0 1.2895 1.6780 89

90 625.35 0.0008 0.0268 1280.0 37.246 293.4 140.1 433.5 1.2926 1.6784 9091 640.28 0.0008 0.0262 1276.7 38.142 294.6 139.5 434.1 1.2957 1.6788 9192 655.47 0.0008 0.0256 1273.5 39.056 295.7 138.9 434.6 1.2988 1.6792 9293 670.94 0.0008 0.0250 1270.2 39.988 296.8 138.3 435.2 1.3018 1.6796 9394 686.67 0.0008 0.0244 1266.9 40.939 298.0 137.7 435.7 1.3049 1.6801 94

95 702.68 0.0008 0.0239 1263.6 41.908 299.1 137.1 436.2 1.3080 1.6805 9596 718.96 0.0008 0.0233 1260.3 42.897 300.2 136.5 436.8 1.3110 1.6809 9697 735.53 0.0008 0.0228 1256.9 43.906 301.4 135.9 437.3 1.3141 1.6813 9798 752.38 0.0008 0.0223 1253.6 44.934 302.5 135.3 437.8 1.3171 1.6817 9899 769.51 0.0008 0.0217 1250.2 45.983 303.7 134.7 438.4 1.3202 1.6821 99

100 786.93 0.0008 0.0213 1246.8 47.053 304.8 134.1 438.9 1.3232 1.6825 100101 804.64 0.0008 0.0208 1243.4 48.144 306.0 133.4 439.4 1.3263 1.6829 101102 822.65 0.0008 0.0203 1239.9 49.257 307.1 132.8 439.9 1.3293 1.6832 102103 840.96 0.0008 0.0198 1236.5 50.392 308.3 132.2 440.4 1.3323 1.6836 103104 859.56 0.0008 0.0194 1233.0 51.550 309.4 131.5 440.9 1.3353 1.6840 104

105 878.47 0.0008 0.0190 1229.5 52.730 310.6 130.9 441.4 1.3383 1.6844 105106 897.69 0.0008 0.0185 1226.0 53.935 311.7 130.2 441.9 1.3413 1.6848 106107 917.22 0.0008 0.0181 1222.4 55.163 312.9 129.6 442.4 1.3443 1.6851 107108 937.07 0.0008 0.0177 1218.8 56.416 314.0 128.9 442.9 1.3473 1.6855 108109 957.23 0.0008 0.0173 1215.2 57.693 315.2 128.2 443.4 1.3503 1.6859 109

110 977.71 0.0008 0.0170 1211.6 58.997 316.4 127.5 443.9 1.3533 1.6862 110111 998.52 0.0008 0.0166 1208.0 60.326 317.5 126.9 444.4 1.3563 1.6866 111112 1019.66 0.0008 0.0162 1204.3 61.683 318.7 126.2 444.9 1.3593 1.6869 112113 1041.12 0.0008 0.0159 1200.6 63.066 319.9 125.5 445.3 1.3623 1.6873 113114 1062.92 0.0008 0.0155 1196.9 64.478 321.0 124.8 445.8 1.3652 1.6876 114

115 1085.05 0.0008 0.0152 1193.1 65.919 322.2 124.1 446.3 1.3682 1.6879 115116 1107.52 0.0008 0.0148 1189.3 67.388 323.4 123.4 446.8 1.3712 1.6882 116117 1130.35 0.0008 0.0145 1185.5 68.888 324.5 122.7 447.2 1.3741 1.6886 117118 1153.52 0.0008 0.0142 1181.7 70.418 325.7 121.9 447.7 1.3771 1.6889 118119 1177.04 0.0008 0.0139 1177.8 71.980 326.9 121.2 448.1 1.3801 1.6892 119

120 1200.91 0.0009 0.0136 1173.9 73.574 328.1 120.5 448.6 1.3830 1.6895 120121 1225.15 0.0009 0.0133 1170.0 75.201 329.3 119.7 449.0 1.3860 1.6898 121122 1249.75 0.0009 0.0130 1166.0 76.862 330.4 119.0 449.4 1.3889 1.6900 122123 1274.71 0.0009 0.0127 1162.0 78.558 331.6 118.2 449.9 1.3919 1.6903 123124 1300.04 0.0009 0.0125 1158.0 80.290 332.8 117.5 450.3 1.3948 1.6906 124

125 1325.74 0.0009 0.0122 1153.9 82.058 334.0 116.7 450.7 1.3978 1.6908 125126 1351.82 0.0009 0.0119 1149.8 83.864 335.2 115.9 451.1 1.4007 1.6911 126127 1378.28 0.0009 0.0117 1145.7 85.708 336.4 115.1 451.5 1.4037 1.6913 127128 1405.13 0.0009 0.0114 1141.5 87.593 337.6 114.3 451.9 1.4066 1.6916 128129 1432.36 0.0009 0.0112 1137.3 89.518 338.8 113.5 452.3 1.4095 1.6918 129

130 1459.98 0.0009 0.0109 1133.0 91.485 340.0 112.7 452.7 1.4125 1.6920 130131 1488.00 0.0009 0.0107 1128.7 93.496 341.2 111.9 453.1 1.4154 1.6922 131132 1516.41 0.0009 0.0105 1124.3 95.552 342.5 111.0 453.5 1.4184 1.6924 132133 1545.23 0.0009 0.0102 1119.9 97.654 343.7 110.2 453.9 1.4213 1.6926 133134 1574.46 0.0009 0.0100 1115.5 99.804 344.9 109.3 454.2 1.4242 1.6927 134

135 1604.10 0.0009 0.0098 1111.0 102.003 346.1 108.5 454.6 1.4272 1.6929 135136 1634.15 0.0009 0.0096 1106.4 104.252 347.4 107.6 454.9 1.4301 1.6930 136137 1664.62 0.0009 0.0094 1101.8 106.554 348.6 106.7 455.3 1.4331 1.6932 137138 1695.52 0.0009 0.0092 1097.2 108.911 349.8 105.8 455.6 1.4360 1.6933 138139 1726.84 0.0009 0.0090 1092.4 111.324 351.1 104.9 455.9 1.4390 1.6934 139

LIQUIDvf

VAPORvg

LIQUID1/vf

VAPOR1/vg

LIQUIDhf

LATENThfg

LIQUIDsf

VAPORsg

ENTROPYkJ/(kg)(K)

VAPORhg

PRESSUREkPa (abs)

TEMP.°C

TEMP.°C

VOLUMEm3/kg

DENSITYkg/m3

ENTHALPYkJ/kg

Table 1 (continued)

HCFC�123 Saturation Properties�Temperature Table

7

Page 10: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

140 1758.60 0.0009 0.0088 1087.7 113.796 352.3 103.9 456.3 1.4419 1.6935 140141 1790.79 0.0009 0.0086 1082.8 116.329 353.6 103.0 456.6 1.4449 1.6936 141142 1823.42 0.0009 0.0084 1077.9 118.924 354.8 102.0 456.9 1.4478 1.6936 142143 1856.50 0.0009 0.0082 1073.0 121.585 356.1 101.1 457.2 1.4508 1.6937 143144 1890.03 0.0009 0.0080 1067.9 124.315 357.4 100.1 457.4 1.4538 1.6937 144

145 1924.01 0.0009 0.0079 1062.8 127.115 358.6 99.1 457.7 1.4568 1.6937 145146 1958.46 0.0009 0.0077 1057.6 129.990 359.9 98.1 458.0 1.4597 1.6937 146147 1993.37 0.0010 0.0075 1052.3 132.943 361.2 97.0 458.2 1.4627 1.6937 147148 2028.74 0.0010 0.0074 1047.0 135.976 362.5 96.0 458.5 1.4657 1.6936 148149 2064.60 0.0010 0.0072 1041.5 139.095 363.8 94.9 458.7 1.4687 1.6936 149

150 2100.93 0.0010 0.0070 1036.0 142.303 365.1 93.8 458.9 1.4718 1.6935 150151 2137.75 0.0010 0.0069 1030.4 145.604 366.4 92.7 459.1 1.4748 1.6934 151152 2175.06 0.0010 0.0067 1024.6 149.005 367.8 91.6 459.3 1.4778 1.6932 152153 2212.87 0.0010 0.0066 1018.8 152.509 369.1 90.4 459.5 1.4809 1.6931 153154 2251.19 0.0010 0.0064 1012.8 156.123 370.4 89.3 459.7 1.4839 1.6929 154

155 2290.01 0.0010 0.0063 1006.7 159.853 371.8 88.1 459.8 1.4870 1.6926 155156 2329.35 0.0010 0.0061 1000.5 163.707 373.1 86.8 460.0 1.4901 1.6924 156157 2369.21 0.0010 0.0060 994.2 167.691 374.5 85.6 460.1 1.4932 1.6921 157158 2409.61 0.0010 0.0058 987.7 171.815 375.9 84.3 460.2 1.4963 1.6918 158159 2450.54 0.0010 0.0057 981.0 176.089 377.3 83.0 460.3 1.4994 1.6914 159

160 2492.01 0.0010 0.0055 974.2 180.521 378.7 81.6 460.3 1.5026 1.6910 160161 2534.04 0.0010 0.0054 967.2 185.126 380.1 80.2 460.3 1.5057 1.6905 161162 2576.63 0.0010 0.0053 960.0 189.915 381.6 78.8 460.4 1.5089 1.6900 162163 2619.80 0.0010 0.0051 952.6 194.904 383.0 77.3 460.3 1.5122 1.6895 163164 2663.54 0.0011 0.0050 945.0 200.110 384.5 75.8 460.3 1.5154 1.6889 164

165 2707.88 0.0011 0.0049 937.2 205.552 386.0 74.3 460.2 1.5187 1.6882 165166 2752.81 0.0011 0.0047 929.0 211.254 387.5 72.7 460.1 1.5220 1.6875 166167 2798.36 0.0011 0.0046 920.6 217.240 389.0 71.0 460.0 1.5254 1.6867 167168 2844.54 0.0011 0.0045 911.9 223.542 390.5 69.3 459.8 1.5288 1.6858 168169 2891.36 0.0011 0.0043 902.8 230.194 392.1 67.5 459.6 1.5322 1.6848 169

170 2938.83 0.0011 0.0042 893.3 237.240 393.7 65.6 459.3 1.5357 1.6837 170171 2986.97 0.0011 0.0041 883.4 244.731 395.3 63.6 458.9 1.5393 1.6825 171172 3035.81 0.0011 0.0040 873.0 252.729 397.0 61.6 458.5 1.5429 1.6811 172173 3085.29 0.0012 0.0038 862.0 261.310 398.7 59.4 458.1 1.5466 1.6796 173174 3135.59 0.0012 0.0037 850.4 270.573 400.4 57.1 457.5 1.5503 1.6780 174

175 3186.64 0.0012 0.0036 838.0 280.640 402.2 54.6 456.8 1.5542 1.6761 175176 3238.47 0.0012 0.0034 824.6 291.678 404.1 52.0 456.1 1.5582 1.6739 176177 3291.12 0.0012 0.0033 810.2 303.909 406.0 49.1 455.1 1.5624 1.6715 177178 3344.62 0.0013 0.0031 794.3 317.649 408.1 46.0 454.0 1.5667 1.6686 178179 3399.02 0.0013 0.0030 776.6 333.370 410.2 42.5 452.7 1.5714 1.6653 179

180 3454.38 0.0013 0.0028 756.3 351.827 412.6 38.5 451.0 1.5764 1.6613 180181 3510.78 0.0014 0.0027 732.2 374.369 415.2 33.8 448.9 1.5819 1.6563 181182 3568.29 0.0014 0.0025 701.5 403.890 418.2 27.8 446.0 1.5886 1.6496 182183 3627.05 0.0015 0.0022 654.7 449.494 422.6 18.9 441.5 1.5979 1.6393 183

LIQUIDvf

VAPORvg

LIQUID1/vf

VAPOR1/vg

LIQUIDhf

LATENThfg

LIQUIDsf

VAPORsg

ENTROPYkJ/(kg)(K)

VAPORhg

PRESSUREkPa (abs)

TEMP.°C

TEMP.°C

VOLUMEm3/kg

DENSITYkg/m3

ENTHALPYkJ/kg

Table 1 (continued)

HCFC�123 Saturation Properties�Temperature Table

8

Page 11: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 20.00 kPa (abs)PRESSURE = 10.00 kPa (abs)

PRESSURE = 40.00 kPa (abs)PRESSURE = 30.00 kPa (abs)

Table 2

–23.68 0.0006 180.5 0.9253 0.7894 1.5177 912.8 SAT LIQ 0.0006 191.1 0.9670 0.8264 1.4822 834.6 –10.41–23.68 1.3433 365.7 1.6679 0.6227 1.1048 121.2 SAT VAP 0.7036 373.5 1.6611 0.6471 1.1043 123.7 –10.41

–20 1.3641 368.0 1.6770 0.6262 1.1032 122.1 — — — — — — –20–15 1.3922 371.1 1.6893 0.6311 1.1013 123.3 — — — — — — –15–10 1.4203 374.3 1.7014 0.6362 1.0995 124.5 0.7048 373.8 1.6621 0.6474 1.1041 123.8 –10

–5 1.4482 377.5 1.7135 0.6414 1.0979 125.7 0.7192 377.0 1.6744 0.6512 1.1018 125.0 –50 1.4760 380.7 1.7254 0.6467 1.0964 126.8 0.7334 380.3 1.6864 0.6553 1.0998 126.2 05 1.5038 384.0 1.7371 0.6521 1.0949 128.0 0.7476 383.6 1.6984 0.6596 1.0980 127.4 5

10 1.5315 387.3 1.7488 0.6576 1.0936 129.1 0.7617 386.9 1.7102 0.6641 1.0963 128.5 1015 1.5591 390.6 1.7604 0.6631 1.0924 130.2 0.7757 390.2 1.7218 0.6689 1.0947 129.7 1520 1.5867 393.9 1.7718 0.6687 1.0912 131.3 0.7897 393.6 1.7334 0.6737 1.0933 130.8 2025 1.6142 397.2 1.7832 0.6742 1.0901 132.4 0.8037 397.0 1.7448 0.6786 1.0920 131.9 2530 1.6417 400.6 1.7944 0.6798 1.0891 133.5 0.8176 400.4 1.7561 0.6837 1.0907 133.0 3035 1.6692 404.0 1.8056 0.6854 1.0881 134.5 0.8315 403.8 1.7674 0.6888 1.0896 134.1 3540 1.6967 407.5 1.8167 0.6910 1.0871 135.6 0.8454 407.3 1.7785 0.6940 1.0885 135.2 4045 1.7241 410.9 1.8277 0.6966 1.0862 136.6 0.8592 410.7 1.7895 0.6992 1.0875 136.2 4550 1.7515 414.4 1.8386 0.7021 1.0853 137.7 0.8730 414.3 1.8005 0.7044 1.0865 137.3 5055 1.7790 418.0 1.8494 0.7076 1.0845 138.7 0.8868 417.8 1.8113 0.7096 1.0856 138.3 5560 1.8062 421.5 1.8601 0.7131 1.0837 139.7 0.9005 421.4 1.8221 0.7149 1.0847 139.4 6065 1.8335 425.1 1.8708 0.7186 1.0829 140.7 0.9143 424.9 1.8328 0.7201 1.0839 140.4 6570 1.8609 428.7 1.8814 0.7240 1.0822 141.7 0.9281 428.6 1.8434 0.7254 1.0831 141.4 7075 1.8883 432.3 1.8919 0.7294 1.0815 142.7 0.9419 432.2 1.8539 0.7306 1.0823 142.4 7580 1.9155 436.0 1.9023 0.7347 1.0808 143.7 0.9555 435.9 1.8644 0.7358 1.0816 143.4 8085 1.9429 439.7 1.9127 0.7400 1.0801 144.7 0.9693 439.6 1.8748 0.7409 1.0809 144.4 8590 1.9703 443.4 1.9230 0.7453 1.0795 145.7 0.9830 443.3 1.8851 0.7461 1.0802 145.4 9095 1.9975 447.1 1.9332 0.7505 1.0789 146.7 0.9967 447.0 1.8953 0.7512 1.0796 146.4 95

100 2.0248 450.9 1.9434 0.7556 1.0783 147.6 1.0106 450.8 1.9055 0.7562 1.0789 147.4 100105 2.0522 454.7 1.9535 0.7607 1.0777 148.6 1.0242 454.6 1.9156 0.7613 1.0783 148.3 105110 2.0793 458.5 1.9635 0.7658 1.0771 149.5 1.0379 458.4 1.9256 0.7662 1.0777 149.3 110115 2.1069 462.4 1.9735 0.7707 1.0765 150.5 1.0515 462.2 1.9356 0.7712 1.0772 150.3 115120 2.1342 466.2 1.9834 0.7757 1.0760 151.4 1.0653 466.1 1.9455 0.7760 1.0766 151.2 120125 2.1615 470.1 1.9932 0.7805 1.0755 152.3 1.0789 470.0 1.9553 0.7809 1.0761 152.2 125130 2.1886 474.0 2.0030 0.7853 1.0750 153.3 1.0926 473.9 1.9651 0.7857 1.0756 153.1 130135 — — — — — — 1.1063 477.9 1.9748 0.7904 1.0750 154.0 135140 — — — — — — 1.1202 481.8 1.9844 0.7950 1.0745 154.9 140

–1.91 0.0007 198.3 0.9939 0.8657 1.4620 794.6 SAT LIQ 0.0007 204.0 1.0145 0.8974 1.4502 768.2 4.51–1.91 0.4821 378.6 1.6585 0.6631 1.1044 125.1 SAT VAP 0.3687 382.5 1.6572 0.6752 1.1048 126.1 4.51

0 0.4858 379.9 1.6631 0.6642 1.1035 125.6 — — — — — — 05 0.4955 383.2 1.6752 0.6674 1.1011 126.8 0.3694 382.8 1.6584 0.6754 1.1045 126.2 5

10 0.5051 386.5 1.6871 0.6709 1.0990 128.0 0.3767 386.2 1.6705 0.6779 1.1020 127.4 1015 0.5146 389.9 1.6989 0.6748 1.0972 129.2 0.3840 389.6 1.6824 0.6809 1.0997 128.7 1520 0.5241 393.3 1.7105 0.6789 1.0955 130.3 0.3912 393.0 1.6941 0.6842 1.0977 129.8 2025 0.5335 396.7 1.7221 0.6832 1.0939 131.5 0.3984 396.4 1.7057 0.6878 1.0959 131.0 2530 0.5429 400.1 1.7335 0.6876 1.0925 132.6 0.4055 399.9 1.7172 0.6917 1.0942 132.1 3035 0.5523 403.6 1.7448 0.6923 1.0911 133.7 0.4126 403.3 1.7285 0.6958 1.0927 133.3 3540 0.5616 407.0 1.7559 0.6970 1.0899 134.8 0.4197 406.8 1.7398 0.7001 1.0914 134.4 4045 0.5709 410.5 1.7670 0.7018 1.0888 135.9 0.4267 410.3 1.7509 0.7045 1.0901 135.5 4550 0.5802 414.1 1.7780 0.7067 1.0877 136.9 0.4338 413.9 1.7619 0.7091 1.0889 136.6 5055 0.5894 417.6 1.7889 0.7117 1.0867 138.0 0.4408 417.4 1.7728 0.7137 1.0878 137.7 5560 0.5987 421.2 1.7997 0.7167 1.0857 139.1 0.4477 421.0 1.7837 0.7185 1.0868 138.7 6065 0.6080 424.8 1.8104 0.7217 1.0848 140.1 0.4547 424.6 1.7944 0.7233 1.0858 139.8 6570 0.6172 428.4 1.8210 0.7267 1.0840 141.1 0.4617 428.2 1.8051 0.7281 1.0849 140.8 7075 0.6264 432.0 1.8316 0.7318 1.0832 142.1 0.4687 431.9 1.8156 0.7330 1.0840 141.9 7580 0.6355 435.7 1.8420 0.7368 1.0824 143.2 0.4755 435.6 1.8261 0.7379 1.0832 142.9 8085 0.6447 439.4 1.8524 0.7419 1.0817 144.2 0.4825 439.3 1.8365 0.7428 1.0824 143.9 8590 0.6540 443.1 1.8628 0.7469 1.0810 145.2 0.4894 443.0 1.8469 0.7477 1.0817 144.9 9095 0.6632 446.9 1.8730 0.7519 1.0803 146.2 0.4964 446.7 1.8571 0.7526 1.0810 145.9 95

100 0.6724 450.7 1.8832 0.7569 1.0796 147.1 0.5033 450.5 1.8673 0.7575 1.0803 146.9 100105 0.6816 454.4 1.8933 0.7618 1.0790 148.1 0.5102 454.3 1.8774 0.7624 1.0797 147.9 105110 0.6907 458.3 1.9033 0.7667 1.0784 149.1 0.5172 458.1 1.8875 0.7672 1.0790 148.9 110115 0.6999 462.1 1.9133 0.7716 1.0778 150.0 0.5240 462.0 1.8974 0.7720 1.0784 149.8 115120 0.7091 466.0 1.9232 0.7764 1.0772 151.0 0.5309 465.9 1.9074 0.7768 1.0778 150.8 120125 0.7182 469.9 1.9331 0.7812 1.0767 152.0 0.5378 469.8 1.9172 0.7816 1.0773 151.8 125130 0.7274 473.8 1.9428 0.7860 1.0761 152.9 0.5448 473.7 1.9270 0.7863 1.0767 152.7 130135 0.7366 477.7 1.9526 0.7907 1.0756 153.8 0.5516 477.6 1.9367 0.7910 1.0762 153.7 135140 0.7458 481.7 1.9622 0.7953 1.0751 154.8 0.5585 481.6 1.9464 0.7956 1.0757 154.6 140145 0.7549 485.7 1.9718 0.7999 1.0746 155.7 0.5655 485.6 1.9560 0.8002 1.0752 155.5 145150 0.7641 489.7 1.9813 0.8044 1.0741 156.6 0.5723 489.6 1.9655 0.8047 1.0747 156.5 150155 — — — — — — 0.5792 493.6 1.9750 0.8092 1.0742 157.4 155

9

Page 12: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 70.00 kPa (abs) PRESSURE = 80.00 kPa (abs)

PRESSURE = 60.00 kPa (abs)PRESSURE = 50.00 kPa (abs)

9.73 0.0007 208.8 1.0314 0.9228 1.4430 748.4 SAT LIQ 0.0007 212.9 1.0459 0.9437 1.4383 732.3 14.169.73 0.2994 385.6 1.6567 0.6851 1.1052 126.8 SAT VAP 0.2525 388.3 1.6565 0.6934 1.1057 127.4 14.16

10 0.2997 385.8 1.6573 0.6852 1.1051 126.9 — — — — — — 1015 0.3056 389.2 1.6693 0.6872 1.1024 128.1 0.2533 388.9 1.6585 0.6936 1.1052 127.6 1520 0.3115 392.7 1.6812 0.6897 1.1001 129.3 0.2583 392.4 1.6705 0.6953 1.1026 128.8 2025 0.3173 396.1 1.6929 0.6926 1.0980 130.5 0.2632 395.8 1.6822 0.6975 1.1002 130.1 2530 0.3231 399.6 1.7044 0.6959 1.0961 131.7 0.2681 399.3 1.6938 0.7002 1.0980 131.2 3035 0.3288 403.1 1.7158 0.6995 1.0944 132.9 0.2729 402.8 1.7053 0.7032 1.0961 132.4 3540 0.3345 406.6 1.7271 0.7033 1.0929 134.0 0.2778 406.4 1.7167 0.7065 1.0944 133.6 4045 0.3402 410.1 1.7383 0.7073 1.0915 135.1 0.2825 409.9 1.7279 0.7102 1.0929 134.7 4550 0.3459 413.7 1.7494 0.7115 1.0902 136.2 0.2873 413.5 1.7390 0.7140 1.0914 135.8 5055 0.3515 417.2 1.7603 0.7159 1.0890 137.3 0.2920 417.1 1.7500 0.7180 1.0901 137.0 5560 0.3572 420.8 1.7712 0.7203 1.0878 138.4 0.2968 420.7 1.7609 0.7222 1.0889 138.0 6065 0.3628 424.4 1.7819 0.7249 1.0868 139.5 0.3015 424.3 1.7717 0.7266 1.0878 139.1 6570 0.3684 428.1 1.7926 0.7295 1.0858 140.5 0.3062 427.9 1.7824 0.7310 1.0868 140.2 7075 0.3740 431.7 1.8032 0.7342 1.0849 141.6 0.3109 431.6 1.7930 0.7355 1.0858 141.3 7580 0.3796 435.4 1.8137 0.7390 1.0840 142.6 0.3155 435.3 1.8035 0.7401 1.0849 142.3 8085 0.3852 439.1 1.8241 0.7438 1.0832 143.6 0.3202 439.0 1.8139 0.7447 1.0840 143.4 8590 0.3907 442.9 1.8345 0.7485 1.0825 144.6 0.3249 442.7 1.8243 0.7494 1.0832 144.4 9095 0.3963 446.6 1.8447 0.7534 1.0817 145.7 0.3296 446.5 1.8346 0.7541 1.0824 145.4 95

100 0.4018 450.4 1.8549 0.7582 1.0810 146.7 0.3342 450.3 1.8448 0.7588 1.0817 146.4 100105 0.4074 454.2 1.8650 0.7630 1.0803 147.7 0.3388 454.1 1.8549 0.7635 1.0810 147.4 105110 0.4130 458.0 1.8751 0.7677 1.0797 148.6 0.3435 457.9 1.8650 0.7683 1.0803 148.4 110115 0.4185 461.9 1.8851 0.7725 1.0790 149.6 0.3482 461.8 1.8750 0.7730 1.0797 149.4 115120 0.4241 465.7 1.8950 0.7772 1.0784 150.6 0.3528 465.6 1.8849 0.7777 1.0791 150.4 120125 0.4296 469.6 1.9049 0.7819 1.0779 151.6 0.3574 469.5 1.8947 0.7823 1.0785 151.4 125130 0.4351 473.6 1.9146 0.7866 1.0773 152.5 0.3621 473.5 1.9045 0.7870 1.0779 152.3 130135 0.4407 477.5 1.9244 0.7913 1.0767 153.5 0.3667 477.4 1.9143 0.7916 1.0773 153.3 135140 0.4462 481.5 1.9340 0.7959 1.0762 154.4 0.3713 481.4 1.9239 0.7961 1.0768 154.3 140145 0.4518 485.5 1.9436 0.8004 1.0757 155.4 0.3760 485.4 1.9335 0.8007 1.0763 155.2 145150 0.4573 489.5 1.9532 0.8049 1.0752 156.3 0.3806 489.4 1.9431 0.8052 1.0757 156.1 150155 0.4628 493.5 1.9627 0.8094 1.0747 157.2 0.3852 493.4 1.9526 0.8096 1.0753 157.1 155160 0.4684 497.6 1.9721 0.8138 1.0742 158.2 0.3898 497.5 1.9620 0.8140 1.0748 158.0 160165 — — — — — — 0.3945 501.6 1.9714 0.8184 1.0743 158.9 165

18.04 0.0007 216.6 1.0587 0.9610 1.4351 718.7 SAT LIQ 0.0007 219.9 1.0701 0.9758 1.4330 706.8 21.4918.04 0.2186 390.7 1.6565 0.7007 1.1063 127.8 SAT VAP 0.1929 392.8 1.6567 0.7072 1.1069 128.2 21.49

20 0.2203 392.0 1.6612 0.7011 1.1051 128.3 — — — — — — 2025 0.2246 395.6 1.6731 0.7026 1.1024 129.6 0.1956 395.3 1.6651 0.7078 1.1048 129.1 2530 0.2288 399.1 1.6848 0.7045 1.1001 130.8 0.1994 398.8 1.6769 0.7091 1.1022 130.3 3035 0.2330 402.6 1.6963 0.7070 1.0979 132.0 0.2031 402.4 1.6885 0.7109 1.0998 131.6 3540 0.2372 406.1 1.7078 0.7099 1.0960 133.2 0.2068 405.9 1.6999 0.7133 1.0977 132.8 4045 0.2413 409.7 1.7190 0.7131 1.0943 134.3 0.2104 409.5 1.7113 0.7160 1.0958 133.9 4550 0.2455 413.3 1.7302 0.7165 1.0928 135.5 0.2141 413.1 1.7225 0.7191 1.0941 135.1 5055 0.2496 416.9 1.7412 0.7203 1.0913 136.6 0.2177 416.7 1.7335 0.7225 1.0926 136.2 5560 0.2536 420.5 1.7521 0.7242 1.0900 137.7 0.2213 420.3 1.7445 0.7262 1.0912 137.4 6065 0.2577 424.1 1.7629 0.7283 1.0889 138.8 0.2249 423.9 1.7553 0.7300 1.0899 138.5 6570 0.2618 427.8 1.7737 0.7325 1.0877 139.9 0.2284 427.6 1.7661 0.7340 1.0887 139.6 7075 0.2658 431.4 1.7843 0.7368 1.0867 141.0 0.2320 431.3 1.7767 0.7381 1.0876 140.7 7580 0.2698 435.1 1.7948 0.7412 1.0858 142.0 0.2355 435.0 1.7873 0.7424 1.0866 141.7 8085 0.2739 438.8 1.8053 0.7457 1.0848 143.1 0.2391 438.7 1.7977 0.7467 1.0857 142.8 8590 0.2779 442.6 1.8156 0.7503 1.0840 144.1 0.2426 442.4 1.8081 0.7512 1.0848 143.9 9095 0.2819 446.3 1.8259 0.7549 1.0832 145.1 0.2462 446.2 1.8184 0.7557 1.0839 144.9 95

100 0.2859 450.1 1.8361 0.7595 1.0824 146.2 0.2497 450.0 1.8286 0.7602 1.0831 145.9 100105 0.2899 453.9 1.8463 0.7641 1.0817 147.2 0.2532 453.8 1.8388 0.7647 1.0824 147.0 105110 0.2939 457.8 1.8564 0.7688 1.0810 148.2 0.2567 457.7 1.8489 0.7693 1.0817 148.0 110115 0.2979 461.6 1.8664 0.7734 1.0803 149.2 0.2602 461.5 1.8589 0.7739 1.0810 149.0 115120 0.3019 465.5 1.8763 0.7781 1.0797 150.2 0.2637 465.4 1.8688 0.7785 1.0803 150.0 120125 0.3059 469.4 1.8861 0.7827 1.0791 151.2 0.2672 469.3 1.8787 0.7831 1.0797 151.0 125130 0.3098 473.3 1.8959 0.7873 1.0785 152.1 0.2707 473.2 1.8885 0.7876 1.0791 152.0 130135 0.3139 477.3 1.9057 0.7919 1.0779 153.1 0.2742 477.2 1.8982 0.7922 1.0785 152.9 135140 0.3178 481.3 1.9153 0.7964 1.0774 154.1 0.2777 481.1 1.9079 0.7967 1.0779 153.9 140145 0.3218 485.2 1.9250 0.8009 1.0768 155.0 0.2812 485.1 1.9175 0.8012 1.0774 154.9 145150 0.3258 489.3 1.9345 0.8054 1.0763 156.0 0.2847 489.2 1.9270 0.8057 1.0768 155.8 150155 0.3298 493.3 1.9440 0.8098 1.0758 156.9 0.2882 493.2 1.9365 0.8101 1.0763 156.8 155160 0.3338 497.4 1.9534 0.8142 1.0753 157.9 0.2917 497.3 1.9460 0.8145 1.0758 157.7 160165 0.3377 501.4 1.9628 0.8186 1.0748 158.8 0.2952 501.3 1.9553 0.8188 1.0753 158.7 165170 0.3417 505.5 1.9721 0.8229 1.0743 159.7 0.2987 505.4 1.9647 0.8231 1.0748 159.6 170175 — — — — — — 0.3022 509.6 1.9739 0.8273 1.0744 160.5 175

10

Page 13: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 100.00 kPa (abs)

PRESSURE = 101.325 kPa (abs)

PRESSURE = 90.00 kPa (abs)

24.62 0.0007 223.0 1.0805 0.9885 1.4317 696.2 SAT LIQ 0.0007 225.9 1.0899 0.9995 1.4308 686.5 27.4824.62 0.1728 394.7 1.6570 0.7131 1.1075 128.5 SAT VAP 0.1565 396.4 1.6573 0.7185 1.1082 128.7 27.48

25 0.1730 395.0 1.6579 0.7131 1.1073 128.6 — — — — — — 2530 0.1764 398.5 1.6698 0.7137 1.1043 129.9 0.1581 398.2 1.6634 0.7185 1.1066 129.4 3035 0.1798 402.1 1.6815 0.7150 1.1017 131.1 0.1611 401.8 1.6751 0.7191 1.1037 130.7 3540 0.1831 405.7 1.6930 0.7168 1.0994 132.3 0.1641 405.4 1.6867 0.7204 1.1012 131.9 4045 0.1864 409.3 1.7044 0.7191 1.0974 133.5 0.1671 409.0 1.6981 0.7222 1.0990 133.1 4550 0.1896 412.9 1.7156 0.7218 1.0955 134.7 0.1701 412.7 1.7094 0.7245 1.0970 134.3 5055 0.1929 416.5 1.7267 0.7248 1.0939 135.9 0.1730 416.3 1.7205 0.7272 1.0952 135.5 5560 0.1961 420.1 1.7377 0.7282 1.0924 137.0 0.1760 419.9 1.7316 0.7302 1.0936 136.7 6065 0.1993 423.8 1.7486 0.7318 1.0910 138.1 0.1789 423.6 1.7425 0.7336 1.0921 137.8 6570 0.2025 427.4 1.7593 0.7355 1.0897 139.3 0.1818 427.3 1.7533 0.7371 1.0908 138.9 7075 0.2057 431.1 1.7700 0.7395 1.0886 140.4 0.1846 431.0 1.7639 0.7409 1.0896 140.1 7580 0.2089 434.8 1.7806 0.7436 1.0875 141.4 0.1875 434.7 1.7745 0.7448 1.0884 141.2 8085 0.2120 438.6 1.7910 0.7478 1.0865 142.5 0.1904 438.4 1.7850 0.7488 1.0874 142.2 8590 0.2152 442.3 1.8015 0.7521 1.0856 143.6 0.1932 442.2 1.7954 0.7530 1.0864 143.3 9095 0.2183 446.1 1.8118 0.7564 1.0847 144.6 0.1961 445.9 1.8058 0.7573 1.0855 144.4 95

100 0.2215 449.9 1.8220 0.7609 1.0839 145.7 0.1989 449.7 1.8160 0.7616 1.0846 145.4 100105 0.2246 453.7 1.8322 0.7654 1.0831 146.7 0.2018 453.6 1.8262 0.7660 1.0838 146.5 105110 0.2278 457.5 1.8422 0.7699 1.0824 147.7 0.2046 457.4 1.8363 0.7704 1.0830 147.5 110115 0.2309 461.4 1.8522 0.7744 1.0816 148.8 0.2074 461.3 1.8463 0.7749 1.0823 148.5 115120 0.2340 465.3 1.8622 0.7789 1.0810 149.8 0.2103 465.1 1.8562 0.7794 1.0816 149.6 120125 0.2372 469.2 1.8721 0.7835 1.0803 150.8 0.2131 469.1 1.8661 0.7839 1.0809 150.6 125130 0.2403 473.1 1.8819 0.7880 1.0797 151.8 0.2159 473.0 1.8759 0.7884 1.0803 151.6 130135 0.2434 477.1 1.8916 0.7925 1.0791 152.8 0.2188 476.9 1.8857 0.7928 1.0797 152.6 135140 0.2465 481.0 1.9013 0.7970 1.0785 153.7 0.2215 480.9 1.8953 0.7973 1.0791 153.6 140145 0.2497 485.0 1.9109 0.8015 1.0779 154.7 0.2244 484.9 1.9050 0.8018 1.0785 154.5 145150 0.2528 489.0 1.9205 0.8059 1.0774 155.7 0.2272 488.9 1.9145 0.8062 1.0779 155.5 150155 0.2559 493.1 1.9299 0.8103 1.0769 156.6 0.2300 493.0 1.9240 0.8106 1.0774 156.5 155160 0.2590 497.1 1.9394 0.8147 1.0763 157.6 0.2328 497.0 1.9335 0.8149 1.0769 157.4 160165 0.2621 501.2 1.9487 0.8190 1.0758 158.5 0.2356 501.1 1.9428 0.8192 1.0764 158.4 165170 0.2652 505.3 1.9581 0.8233 1.0754 159.5 0.2384 505.2 1.9522 0.8235 1.0759 159.3 170175 0.2683 509.5 1.9673 0.8275 1.0749 160.4 0.2412 509.4 1.9614 0.8277 1.0754 160.3 175180 — — — — — — 0.2441 513.5 1.9706 0.8319 1.0749 161.2 180

27.84 0.0007 226.2 1.0911 1.0008 1.4307 685.3 SAT LIQ 0.0007 228.5 1.0987 1.0092 1.4303 677.6 30.1227.84 0.1546 396.7 1.6574 0.7191 1.1083 128.8 SAT VAP 0.1431 398.1 1.6578 0.7234 1.1089 128.9 30.12

30 0.1559 398.2 1.6625 0.7191 1.1069 129.3 — — — — — — 3035 0.1589 401.8 1.6743 0.7197 1.1040 130.6 0.1459 401.6 1.6693 0.7234 1.1058 130.2 3540 0.1619 405.4 1.6859 0.7209 1.1014 131.8 0.1486 405.2 1.6809 0.7241 1.1031 131.5 4045 0.1649 409.0 1.6973 0.7226 1.0992 133.1 0.1514 408.8 1.6924 0.7254 1.1006 132.7 4550 0.1678 412.6 1.7086 0.7249 1.0972 134.3 0.1541 412.5 1.7037 0.7273 1.0985 133.9 5055 0.1707 416.3 1.7198 0.7275 1.0954 135.5 0.1568 416.1 1.7149 0.7296 1.0965 135.1 5560 0.1736 419.9 1.7308 0.7305 1.0937 136.6 0.1595 419.8 1.7260 0.7324 1.0948 136.3 6065 0.1765 423.6 1.7417 0.7338 1.0923 137.8 0.1621 423.4 1.7369 0.7354 1.0933 137.5 6570 0.1793 427.2 1.7525 0.7373 1.0909 138.9 0.1648 427.1 1.7477 0.7387 1.0918 138.6 7075 0.1822 430.9 1.7632 0.7410 1.0897 140.0 0.1674 430.8 1.7584 0.7423 1.0905 139.7 7580 0.1850 434.7 1.7738 0.7449 1.0885 141.1 0.1701 434.5 1.7691 0.7460 1.0893 140.9 8085 0.1878 438.4 1.7843 0.7490 1.0875 142.2 0.1727 438.3 1.7796 0.7499 1.0882 142.0 8590 0.1907 442.1 1.7947 0.7531 1.0865 143.3 0.1753 442.0 1.7900 0.7539 1.0872 143.0 9095 0.1935 445.9 1.8050 0.7574 1.0856 144.3 0.1779 445.8 1.8003 0.7581 1.0863 144.1 95

100 0.1963 449.7 1.8153 0.7617 1.0847 145.4 0.1805 449.6 1.8106 0.7623 1.0854 145.2 100105 0.1991 453.5 1.8254 0.7661 1.0839 146.5 0.1831 453.4 1.8208 0.7666 1.0845 146.2 105110 0.2019 457.4 1.8355 0.7705 1.0831 147.5 0.1857 457.3 1.8309 0.7710 1.0837 147.3 110115 0.2047 461.2 1.8456 0.7750 1.0824 148.5 0.1883 461.1 1.8409 0.7754 1.0830 148.3 115120 0.2075 465.1 1.8555 0.7794 1.0817 149.5 0.1908 465.0 1.8508 0.7798 1.0823 149.4 120125 0.2103 469.0 1.8654 0.7839 1.0810 150.5 0.1934 468.9 1.8607 0.7843 1.0816 150.4 125130 0.2131 473.0 1.8752 0.7884 1.0804 151.6 0.1960 472.9 1.8705 0.7887 1.0809 151.4 130135 0.2159 476.9 1.8849 0.7929 1.0798 152.5 0.1986 476.8 1.8803 0.7932 1.0803 152.4 135140 0.2186 480.9 1.8946 0.7973 1.0792 153.5 0.2012 480.8 1.8900 0.7976 1.0797 153.4 140145 0.2214 484.9 1.9042 0.8018 1.0786 154.5 0.2037 484.8 1.8996 0.8020 1.0791 154.4 145150 0.2242 488.9 1.9138 0.8062 1.0780 155.5 0.2063 488.8 1.9092 0.8064 1.0785 155.4 150155 0.2270 493.0 1.9233 0.8106 1.0775 156.5 0.2089 492.9 1.9187 0.8108 1.0779 156.3 155160 0.2297 497.0 1.9327 0.8150 1.0769 157.4 0.2114 496.9 1.9281 0.8152 1.0774 157.3 160165 0.2325 501.1 1.9421 0.8193 1.0764 158.4 0.2140 501.0 1.9375 0.8195 1.0769 158.2 165170 0.2353 505.2 1.9514 0.8235 1.0759 159.3 0.2165 505.1 1.9468 0.8237 1.0764 159.2 170175 0.2381 509.3 1.9607 0.8278 1.0754 160.3 0.2191 509.3 1.9561 0.8280 1.0759 160.1 175180 0.2408 513.5 1.9699 0.8320 1.0750 161.2 0.2217 513.4 1.9653 0.8321 1.0754 161.1 180185 — — — — — — 0.2242 517.6 1.9744 0.8363 1.0749 162.0 185

PRESSURE = 110.00 kPa (abs)

11

Page 14: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 140.00 kPa (abs) PRESSURE = 150.00 kPa (abs)

PRESSURE = 130.00 kPa (abs)PRESSURE = 120.00 kPa (abs)

32.58 0.0007 231.0 1.1069 1.0178 1.4300 669.3 SAT LIQ 0.0007 233.4 1.1146 1.0255 1.4300 661.4 34.8932.58 0.1319 399.6 1.6582 0.7280 1.1096 129.1 SAT VAP 0.1223 401.0 1.6586 0.7323 1.1103 129.2 34.89

35 0.1331 401.3 1.6639 0.7278 1.1080 129.7 0.1224 401.0 1.6589 0.7323 1.1102 129.3 3540 0.1357 405.0 1.6756 0.7279 1.1050 131.0 0.1248 404.7 1.6707 0.7318 1.1070 130.6 4045 0.1383 408.6 1.6872 0.7287 1.1023 132.3 0.1271 408.4 1.6823 0.7321 1.1041 131.9 4550 0.1408 412.2 1.6985 0.7302 1.1000 133.6 0.1295 412.0 1.6937 0.7331 1.1016 133.2 5055 0.1433 415.9 1.7098 0.7321 1.0979 134.8 0.1318 415.7 1.7050 0.7347 1.0994 134.4 5560 0.1457 419.6 1.7209 0.7345 1.0961 136.0 0.1341 419.4 1.7161 0.7367 1.0974 135.6 6065 0.1482 423.2 1.7318 0.7373 1.0944 137.1 0.1364 423.1 1.7271 0.7392 1.0956 136.8 6570 0.1506 426.9 1.7427 0.7404 1.0929 138.3 0.1387 426.8 1.7380 0.7420 1.0940 138.0 7075 0.1531 430.6 1.7534 0.7437 1.0915 139.4 0.1409 430.5 1.7487 0.7452 1.0926 139.1 7580 0.1555 434.4 1.7640 0.7473 1.0903 140.6 0.1432 434.2 1.7594 0.7485 1.0912 140.3 8085 0.1579 438.1 1.7746 0.7510 1.0891 141.7 0.1454 438.0 1.7699 0.7521 1.0900 141.4 8590 0.1603 441.9 1.7850 0.7549 1.0881 142.8 0.1477 441.7 1.7804 0.7559 1.0889 142.5 9095 0.1627 445.7 1.7953 0.7589 1.0871 143.9 0.1499 445.5 1.7907 0.7598 1.0879 143.6 95

100 0.1651 449.5 1.8056 0.7631 1.0861 144.9 0.1521 449.3 1.8010 0.7638 1.0869 144.7 100105 0.1675 453.3 1.8158 0.7673 1.0853 146.0 0.1543 453.2 1.8112 0.7680 1.0860 145.8 105110 0.1699 457.1 1.8259 0.7716 1.0844 147.1 0.1565 457.0 1.8213 0.7722 1.0852 146.8 110115 0.1723 461.0 1.8359 0.7759 1.0837 148.1 0.1587 460.9 1.8314 0.7764 1.0843 147.9 115120 0.1747 464.9 1.8459 0.7803 1.0829 149.1 0.1609 464.8 1.8413 0.7807 1.0836 148.9 120125 0.1770 468.8 1.8558 0.7847 1.0822 150.2 0.1631 468.7 1.8512 0.7851 1.0829 150.0 125130 0.1794 472.8 1.8656 0.7891 1.0815 151.2 0.1653 472.6 1.8610 0.7895 1.0822 151.0 130135 0.1818 476.7 1.8754 0.7935 1.0809 152.2 0.1675 476.6 1.8708 0.7939 1.0815 152.0 135140 0.1841 480.7 1.8850 0.7979 1.0803 153.2 0.1697 480.6 1.8805 0.7982 1.0808 153.0 140145 0.1865 484.7 1.8947 0.8023 1.0796 154.2 0.1719 484.6 1.8901 0.8026 1.0802 154.0 145150 0.1889 488.7 1.9042 0.8067 1.0791 155.2 0.1741 488.6 1.8997 0.8070 1.0796 155.0 150155 0.1912 492.8 1.9137 0.8111 1.0785 156.2 0.1763 492.6 1.9092 0.8113 1.0791 156.0 155160 0.1936 496.8 1.9232 0.8154 1.0779 157.1 0.1785 496.7 1.9186 0.8156 1.0785 157.0 160165 0.1959 500.9 1.9326 0.8197 1.0774 158.1 0.1806 500.8 1.9280 0.8199 1.0779 158.0 165170 0.1983 505.0 1.9419 0.8240 1.0769 159.1 0.1829 504.9 1.9374 0.8242 1.0774 158.9 170175 0.2006 509.2 1.9511 0.8282 1.0764 160.0 0.1850 509.0 1.9466 0.8284 1.0769 159.9 175180 0.2030 513.3 1.9604 0.8323 1.0759 161.0 0.1872 513.2 1.9558 0.8326 1.0764 160.8 180185 0.2054 517.5 1.9695 0.8365 1.0754 161.9 0.1894 517.4 1.9650 0.8367 1.0759 161.8 185

37.06 0.0007 235.6 1.1218 1.0324 1.4301 654.1 SAT LIQ 0.0007 237.7 1.1286 1.0386 1.4303 647.1 39.1137.06 0.1141 402.3 1.6591 0.7363 1.1110 129.4 SAT VAP 0.1069 403.6 1.6596 0.7401 1.1118 129.5 39.11

40 0.1154 404.5 1.6661 0.7358 1.1090 130.2 0.1072 404.2 1.6617 0.7399 1.1112 129.7 4045 0.1176 408.1 1.6777 0.7356 1.1059 131.5 0.1094 407.9 1.6734 0.7391 1.1078 131.0 4550 0.1198 411.8 1.6892 0.7361 1.1032 132.8 0.1114 411.6 1.6849 0.7392 1.1049 132.4 5055 0.1220 415.5 1.7005 0.7373 1.1008 134.0 0.1135 415.3 1.6963 0.7399 1.1023 133.6 5560 0.1241 419.2 1.7117 0.7390 1.0987 135.2 0.1155 419.0 1.7075 0.7413 1.1001 134.9 6065 0.1263 422.9 1.7227 0.7412 1.0968 136.5 0.1175 422.7 1.7185 0.7432 1.0981 136.1 6570 0.1284 426.6 1.7336 0.7438 1.0951 137.6 0.1195 426.4 1.7295 0.7455 1.0963 137.3 7075 0.1305 430.3 1.7444 0.7467 1.0936 138.8 0.1215 430.2 1.7403 0.7482 1.0947 138.5 7580 0.1326 434.1 1.7550 0.7498 1.0922 140.0 0.1235 433.9 1.7510 0.7512 1.0932 139.7 8085 0.1347 437.8 1.7656 0.7533 1.0909 141.1 0.1254 437.7 1.7615 0.7544 1.0919 140.8 8590 0.1368 441.6 1.7761 0.7569 1.0898 142.2 0.1274 441.5 1.7720 0.7579 1.0907 142.0 9095 0.1389 445.4 1.7864 0.7607 1.0887 143.3 0.1293 445.3 1.7824 0.7616 1.0895 143.1 95

100 0.1409 449.2 1.7967 0.7646 1.0877 144.4 0.1313 449.1 1.7927 0.7654 1.0885 144.2 100105 0.1430 453.0 1.8069 0.7686 1.0868 145.5 0.1332 452.9 1.8029 0.7693 1.0875 145.3 105110 0.1451 456.9 1.8171 0.7728 1.0859 146.6 0.1351 456.8 1.8131 0.7734 1.0866 146.4 110115 0.1471 460.8 1.8271 0.7770 1.0850 147.7 0.1371 460.6 1.8231 0.7775 1.0857 147.5 115120 0.1492 464.7 1.8371 0.7812 1.0843 148.7 0.1390 464.5 1.8331 0.7817 1.0849 148.5 120125 0.1512 468.6 1.8470 0.7855 1.0835 149.8 0.1409 468.5 1.8430 0.7860 1.0842 149.6 125130 0.1533 472.5 1.8568 0.7899 1.0828 150.8 0.1428 472.4 1.8528 0.7902 1.0834 150.6 130135 0.1553 476.5 1.8666 0.7942 1.0821 151.8 0.1448 476.4 1.8626 0.7945 1.0827 151.7 135140 0.1574 480.5 1.8763 0.7986 1.0814 152.9 0.1467 480.3 1.8723 0.7989 1.0820 152.7 140145 0.1594 484.5 1.8859 0.8029 1.0808 153.9 0.1486 484.4 1.8819 0.8032 1.0814 153.7 145150 0.1615 488.5 1.8955 0.8072 1.0802 154.9 0.1505 488.4 1.8915 0.8075 1.0808 154.7 150155 0.1635 492.5 1.9050 0.8116 1.0796 155.9 0.1524 492.4 1.9010 0.8118 1.0802 155.7 155160 0.1655 496.6 1.9144 0.8159 1.0790 156.9 0.1543 496.5 1.9105 0.8161 1.0796 156.7 160165 0.1676 500.7 1.9238 0.8202 1.0785 157.8 0.1562 500.6 1.9199 0.8204 1.0790 157.7 165170 0.1696 504.8 1.9331 0.8244 1.0779 158.8 0.1581 504.7 1.9292 0.8246 1.0785 158.7 170175 0.1716 508.9 1.9424 0.8286 1.0774 159.8 0.1600 508.8 1.9385 0.8288 1.0779 159.6 175180 0.1737 513.1 1.9516 0.8328 1.0769 160.7 0.1619 513.0 1.9477 0.8330 1.0774 160.6 180185 0.1757 517.3 1.9608 0.8369 1.0764 161.7 0.1638 517.2 1.9569 0.8371 1.0769 161.6 185190 0.1777 521.5 1.9699 0.8410 1.0759 162.6 0.1657 521.4 1.9660 0.8412 1.0764 162.5 190

12

Page 15: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 170.00 kPa (abs)PRESSURE = 160.00 kPa (abs)

PRESSURE = 180.00 kPa (abs) PRESSURE = 190.00 kPa (abs)

41.06 0.0007 239.8 1.1351 1.0443 1.4306 640.4 SAT LIQ 0.0007 241.7 1.1412 1.0495 1.4310 634.0 42.9241.06 0.1006 404.7 1.6601 0.7437 1.1126 129.5 SAT VAP 0.0949 405.9 1.6606 0.7472 1.1133 129.6 42.92

45 0.1021 407.7 1.6693 0.7428 1.1098 130.6 0.0957 407.4 1.6655 0.7465 1.1118 130.2 4550 0.1041 411.4 1.6809 0.7423 1.1066 131.9 0.0976 411.2 1.6771 0.7456 1.1084 131.5 5055 0.1060 415.1 1.6923 0.7427 1.1039 133.2 0.0994 414.9 1.6886 0.7455 1.1055 132.9 5560 0.1079 418.8 1.7036 0.7437 1.1015 134.5 0.1013 418.6 1.6998 0.7461 1.1029 134.2 6065 0.1098 422.5 1.7147 0.7452 1.0994 135.8 0.1031 422.3 1.7110 0.7474 1.1007 135.4 6570 0.1117 426.3 1.7256 0.7473 1.0975 137.0 0.1049 426.1 1.7219 0.7491 1.0987 136.7 7075 0.1136 430.0 1.7364 0.7497 1.0958 138.2 0.1066 429.8 1.7328 0.7513 1.0969 137.9 7580 0.1155 433.8 1.7471 0.7525 1.0942 139.4 0.1084 433.6 1.7435 0.7539 1.0953 139.1 8085 0.1173 437.5 1.7577 0.7556 1.0928 140.5 0.1101 437.4 1.7542 0.7568 1.0938 140.2 8590 0.1192 441.3 1.7682 0.7589 1.0916 141.7 0.1119 441.2 1.7647 0.7600 1.0925 141.4 9095 0.1210 445.1 1.7786 0.7625 1.0904 142.8 0.1136 445.0 1.7751 0.7634 1.0912 142.6 95

100 0.1228 448.9 1.7890 0.7662 1.0893 143.9 0.1154 448.8 1.7854 0.7670 1.0901 143.7 100105 0.1247 452.8 1.7992 0.7700 1.0883 145.0 0.1171 452.6 1.7956 0.7707 1.0891 144.8 105110 0.1265 456.6 1.8093 0.7740 1.0873 146.1 0.1188 456.5 1.8058 0.7746 1.0881 145.9 110115 0.1283 460.5 1.8194 0.7781 1.0864 147.2 0.1205 460.4 1.8159 0.7786 1.0872 147.0 115120 0.1301 464.4 1.8294 0.7822 1.0856 148.3 0.1222 464.3 1.8258 0.7827 1.0863 148.1 120125 0.1319 468.3 1.8393 0.7864 1.0848 149.4 0.1239 468.2 1.8358 0.7868 1.0855 149.2 125130 0.1337 472.3 1.8491 0.7906 1.0841 150.4 0.1257 472.2 1.8456 0.7910 1.0847 150.2 130135 0.1355 476.2 1.8589 0.7949 1.0833 151.5 0.1274 476.1 1.8554 0.7953 1.0840 151.3 135140 0.1373 480.2 1.8686 0.7992 1.0826 152.5 0.1290 480.1 1.8651 0.7995 1.0833 152.3 140145 0.1391 484.2 1.8782 0.8035 1.0820 153.5 0.1308 484.1 1.8747 0.8038 1.0826 153.4 145150 0.1409 488.3 1.8878 0.8078 1.0813 154.5 0.1325 488.2 1.8843 0.8081 1.0819 154.4 150155 0.1427 492.3 1.8973 0.8121 1.0807 155.6 0.1342 492.2 1.8938 0.8124 1.0813 155.4 155160 0.1445 496.4 1.9068 0.8164 1.0801 156.6 0.1358 496.3 1.9033 0.8166 1.0807 156.4 160165 0.1463 500.5 1.9162 0.8206 1.0795 157.6 0.1375 500.4 1.9127 0.8209 1.0801 157.4 165170 0.1481 504.6 1.9255 0.8249 1.0790 158.5 0.1392 504.5 1.9220 0.8251 1.0795 158.4 170175 0.1499 508.7 1.9348 0.8290 1.0784 159.5 0.1409 508.6 1.9313 0.8293 1.0789 159.4 175180 0.1517 512.9 1.9440 0.8332 1.0779 160.5 0.1426 512.8 1.9405 0.8334 1.0784 160.4 180185 0.1535 517.1 1.9532 0.8373 1.0774 161.5 0.1443 517.0 1.9497 0.8375 1.0779 161.3 185190 0.1552 521.3 1.9623 0.8414 1.0769 162.4 0.1460 521.2 1.9588 0.8416 1.0773 162.3 190195 0.1570 525.5 1.9713 0.8454 1.0764 163.4 0.1477 525.4 1.9679 0.8456 1.0768 163.3 195

44.7 0.0007 243.6 1.1471 1.0543 1.4314 627.9 SAT LIQ 0.0007 245.4 1.1527 1.0587 1.4319 622.0 46.444.7 0.0899 407.0 1.6611 0.7505 1.1141 129.7 SAT VAP 0.0854 408.0 1.6616 0.7536 1.1149 129.7 46.4

45 0.0901 407.2 1.6618 0.7504 1.1139 129.7 — — — — — — 4550 0.0918 410.9 1.6735 0.7489 1.1103 131.1 0.0867 410.7 1.6700 0.7523 1.1122 130.7 5055 0.0936 414.7 1.6850 0.7483 1.1072 132.5 0.0884 414.5 1.6816 0.7513 1.1089 132.1 5560 0.0953 418.4 1.6963 0.7486 1.1044 133.8 0.0900 418.2 1.6929 0.7511 1.1060 133.4 6065 0.0970 422.2 1.7075 0.7495 1.1020 135.1 0.0917 422.0 1.7041 0.7517 1.1034 134.7 6570 0.0987 425.9 1.7185 0.7510 1.0999 136.3 0.0933 425.7 1.7152 0.7529 1.1012 136.0 7075 0.1004 429.7 1.7294 0.7530 1.0980 137.6 0.0949 429.5 1.7261 0.7546 1.0992 137.2 7580 0.1021 433.4 1.7401 0.7553 1.0963 138.8 0.0965 433.3 1.7368 0.7568 1.0974 138.5 8085 0.1038 437.2 1.7507 0.7581 1.0948 140.0 0.0981 437.1 1.7475 0.7593 1.0958 139.7 8590 0.1054 441.0 1.7613 0.7611 1.0934 141.1 0.0996 440.9 1.7581 0.7622 1.0943 140.9 9095 0.1071 444.8 1.7717 0.7643 1.0921 142.3 0.1012 444.7 1.7685 0.7653 1.0930 142.0 95

100 0.1087 448.7 1.7820 0.7678 1.0909 143.4 0.1028 448.5 1.7788 0.7687 1.0918 143.2 100105 0.1104 452.5 1.7923 0.7715 1.0898 144.6 0.1043 452.4 1.7891 0.7722 1.0906 144.3 105110 0.1120 456.4 1.8024 0.7753 1.0888 145.7 0.1059 456.3 1.7993 0.7759 1.0896 145.4 110115 0.1136 460.3 1.8125 0.7792 1.0879 146.8 0.1074 460.1 1.8093 0.7798 1.0886 146.6 115120 0.1152 464.2 1.8225 0.7832 1.0870 147.9 0.1090 464.1 1.8194 0.7837 1.0877 147.7 120125 0.1169 468.1 1.8324 0.7873 1.0862 149.0 0.1105 468.0 1.8293 0.7878 1.0868 148.8 125130 0.1185 472.0 1.8423 0.7914 1.0854 150.0 0.1121 471.9 1.8391 0.7919 1.0860 149.8 130135 0.1201 476.0 1.8521 0.7956 1.0846 151.1 0.1136 475.9 1.8489 0.7960 1.0852 150.9 135140 0.1217 480.0 1.8618 0.7999 1.0839 152.1 0.1151 479.9 1.8586 0.8002 1.0845 152.0 140145 0.1233 484.0 1.8714 0.8041 1.0832 153.2 0.1167 483.9 1.8683 0.8044 1.0838 153.0 145150 0.1249 488.0 1.8810 0.8084 1.0825 154.2 0.1182 487.9 1.8779 0.8087 1.0831 154.1 150155 0.1265 492.1 1.8905 0.8126 1.0819 155.2 0.1197 492.0 1.8874 0.8129 1.0824 155.1 155160 0.1281 496.2 1.9000 0.8169 1.0812 156.3 0.1213 496.1 1.8969 0.8171 1.0818 156.1 160165 0.1297 500.3 1.9094 0.8211 1.0806 157.3 0.1228 500.2 1.9063 0.8214 1.0812 157.1 165170 0.1314 504.4 1.9187 0.8253 1.0800 158.3 0.1243 504.3 1.9156 0.8256 1.0806 158.1 170175 0.1329 508.5 1.9280 0.8295 1.0795 159.3 0.1258 508.4 1.9249 0.8297 1.0800 159.1 175180 0.1345 512.7 1.9372 0.8336 1.0789 160.2 0.1273 512.6 1.9341 0.8339 1.0794 160.1 180185 0.1361 516.9 1.9464 0.8378 1.0784 161.2 0.1289 516.8 1.9433 0.8380 1.0789 161.1 185190 0.1378 521.1 1.9555 0.8418 1.0778 162.2 0.1304 521.0 1.9524 0.8421 1.0783 162.1 190195 0.1393 525.3 1.9646 0.8459 1.0773 163.2 0.1319 525.2 1.9615 0.8461 1.0778 163.1 195200 — — — — — — 0.1334 529.4 1.9705 0.8501 1.0773 164.0 200

13

Page 16: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 220.00 kPa (abs) PRESSURE = 230.00 kPa (abs)

PRESSURE = 210.00 kPa (abs)PRESSURE = 200.00 kPa (abs)

48.03 0.0007 247.1 1.1581 1.0627 1.4325 616.3 SAT LIQ 0.0007 248.8 1.1633 1.0665 1.4331 610.8 49.648.03 0.0814 409.0 1.6621 0.7567 1.1157 129.7 SAT VAP 0.0777 409.9 1.6626 0.7596 1.1166 129.7 49.6

50 0.0820 410.5 1.6667 0.7558 1.1142 130.3 0.0778 410.2 1.6635 0.7594 1.1162 129.9 5055 0.0836 414.3 1.6783 0.7543 1.1106 131.7 0.0794 414.0 1.6752 0.7574 1.1124 131.3 5560 0.0852 418.0 1.6897 0.7537 1.1075 133.0 0.0809 417.8 1.6866 0.7564 1.1092 132.6 6065 0.0868 421.8 1.7009 0.7540 1.1048 134.4 0.0824 421.6 1.6979 0.7563 1.1063 134.0 6570 0.0884 425.6 1.7120 0.7549 1.1025 135.6 0.0839 425.4 1.7090 0.7569 1.1038 135.3 7075 0.0899 429.3 1.7229 0.7563 1.1004 136.9 0.0854 429.2 1.7199 0.7581 1.1016 136.6 7580 0.0914 433.1 1.7337 0.7583 1.0985 138.2 0.0868 433.0 1.7308 0.7598 1.0996 137.8 8085 0.0929 436.9 1.7444 0.7606 1.0968 139.4 0.0883 436.8 1.7415 0.7619 1.0978 139.1 8590 0.0944 440.7 1.7550 0.7633 1.0953 140.6 0.0897 440.6 1.7520 0.7644 1.0962 140.3 9095 0.0959 444.6 1.7654 0.7663 1.0939 141.8 0.0912 444.4 1.7625 0.7673 1.0948 141.5 95

100 0.0974 448.4 1.7758 0.7695 1.0926 142.9 0.0926 448.3 1.7729 0.7704 1.0935 142.7 100105 0.0989 452.3 1.7861 0.7730 1.0914 144.1 0.0940 452.1 1.7832 0.7737 1.0923 143.8 105110 0.1004 456.1 1.7962 0.7766 1.0904 145.2 0.0954 456.0 1.7933 0.7773 1.0911 145.0 110115 0.1019 460.0 1.8063 0.7804 1.0894 146.3 0.0969 459.9 1.8034 0.7810 1.0901 146.1 115120 0.1034 463.9 1.8163 0.7842 1.0884 147.4 0.0983 463.8 1.8135 0.7848 1.0891 147.2 120125 0.1048 467.9 1.8263 0.7882 1.0875 148.5 0.0997 467.7 1.8234 0.7887 1.0882 148.3 125130 0.1063 471.8 1.8361 0.7923 1.0867 149.6 0.1011 471.7 1.8333 0.7927 1.0873 149.4 130135 0.1078 475.8 1.8459 0.7964 1.0859 150.7 0.1025 475.7 1.8431 0.7968 1.0865 150.5 135140 0.1092 479.8 1.8556 0.8006 1.0851 151.8 0.1039 479.7 1.8528 0.8009 1.0857 151.6 140145 0.1107 483.8 1.8653 0.8048 1.0844 152.8 0.1053 483.7 1.8624 0.8051 1.0850 152.7 145150 0.1121 487.8 1.8749 0.8090 1.0837 153.9 0.1067 487.7 1.8720 0.8093 1.0843 153.7 150155 0.1136 491.9 1.8844 0.8132 1.0830 154.9 0.1081 491.8 1.8816 0.8135 1.0836 154.8 155160 0.1150 496.0 1.8939 0.8174 1.0824 156.0 0.1094 495.8 1.8911 0.8177 1.0829 155.8 160165 0.1165 500.1 1.9033 0.8216 1.0817 157.0 0.1108 499.9 1.9005 0.8219 1.0823 156.8 165170 0.1180 504.2 1.9126 0.8258 1.0811 158.0 0.1122 504.1 1.9098 0.8260 1.0816 157.9 170175 0.1194 508.3 1.9219 0.8300 1.0805 159.0 0.1136 508.2 1.9191 0.8302 1.0810 158.9 175180 0.1209 512.5 1.9312 0.8341 1.0799 160.0 0.1150 512.4 1.9283 0.8343 1.0804 159.9 180185 0.1223 516.7 1.9403 0.8382 1.0794 161.0 0.1164 516.5 1.9375 0.8384 1.0799 160.9 185190 0.1238 520.9 1.9495 0.8423 1.0788 162.0 0.1177 520.7 1.9466 0.8425 1.0793 161.9 190195 0.1252 525.1 1.9585 0.8463 1.0783 162.9 0.1191 525.0 1.9557 0.8465 1.0787 162.8 195200 0.1266 529.3 1.9675 0.8503 1.0777 163.9 0.1205 529.2 1.9647 0.8505 1.0782 163.8 200

51.11 0.0007 250.4 1.1683 1.0700 1.4336 605.5 SAT LIQ 0.0007 252.0 1.1731 1.0732 1.4343 600.3 52.5851.11 0.0743 410.9 1.6631 0.7624 1.1174 129.7 SAT VAP 0.0712 411.7 1.6636 0.7651 1.1182 129.7 52.58

55 0.0755 413.8 1.6721 0.7606 1.1143 130.9 0.0719 413.6 1.6692 0.7638 1.1162 130.5 5560 0.0770 417.6 1.6836 0.7591 1.1108 132.3 0.0734 417.4 1.6808 0.7619 1.1125 131.9 6065 0.0784 421.4 1.6949 0.7586 1.1078 133.6 0.0748 421.2 1.6921 0.7610 1.1093 133.3 6570 0.0798 425.2 1.7061 0.7589 1.1051 135.0 0.0761 425.0 1.7033 0.7610 1.1065 134.6 7075 0.0813 429.0 1.7171 0.7598 1.1028 136.3 0.0775 428.8 1.7143 0.7616 1.1041 135.9 7580 0.0827 432.8 1.7279 0.7613 1.1007 137.5 0.0789 432.6 1.7252 0.7629 1.1019 137.2 8085 0.0841 436.6 1.7386 0.7633 1.0989 138.8 0.0802 436.5 1.7359 0.7646 1.1000 138.5 8590 0.0855 440.4 1.7492 0.7656 1.0972 140.0 0.0815 440.3 1.7465 0.7668 1.0982 139.7 9095 0.0868 444.3 1.7597 0.7683 1.0957 141.2 0.0829 444.1 1.7570 0.7694 1.0967 140.9 95

100 0.0882 448.1 1.7701 0.7713 1.0943 142.4 0.0842 448.0 1.7674 0.7722 1.0952 142.1 100105 0.0896 452.0 1.7804 0.7745 1.0931 143.6 0.0855 451.8 1.7777 0.7753 1.0939 143.3 105110 0.0909 455.9 1.7906 0.7780 1.0919 144.7 0.0868 455.7 1.7879 0.7787 1.0927 144.5 110115 0.0923 459.8 1.8007 0.7816 1.0909 145.9 0.0881 459.6 1.7980 0.7822 1.0916 145.7 115120 0.0936 463.7 1.8107 0.7853 1.0899 147.0 0.0894 463.6 1.8081 0.7859 1.0906 146.8 120125 0.0950 467.6 1.8207 0.7892 1.0889 148.1 0.0907 467.5 1.8180 0.7897 1.0896 147.9 125130 0.0963 471.6 1.8305 0.7931 1.0880 149.2 0.0920 471.5 1.8279 0.7936 1.0887 149.0 130135 0.0977 475.5 1.8403 0.7972 1.0872 150.3 0.0933 475.4 1.8377 0.7976 1.0878 150.2 135140 0.0990 479.5 1.8501 0.8013 1.0864 151.4 0.0946 479.4 1.8474 0.8016 1.0870 151.2 140145 0.1003 483.6 1.8597 0.8054 1.0856 152.5 0.0958 483.4 1.8571 0.8057 1.0862 152.3 145150 0.1017 487.6 1.8693 0.8096 1.0849 153.6 0.0971 487.5 1.8667 0.8099 1.0855 153.4 150155 0.1030 491.7 1.8789 0.8137 1.0842 154.6 0.0984 491.5 1.8762 0.8140 1.0848 154.5 155160 0.1044 495.7 1.8883 0.8179 1.0835 155.7 0.0997 495.6 1.8857 0.8182 1.0841 155.5 160165 0.1057 499.8 1.8977 0.8221 1.0828 156.7 0.1010 499.7 1.8951 0.8224 1.0834 156.6 165170 0.1070 504.0 1.9071 0.8263 1.0822 157.7 0.1022 503.9 1.9045 0.8265 1.0827 157.6 170175 0.1083 508.1 1.9164 0.8304 1.0816 158.7 0.1035 508.0 1.9138 0.8307 1.0821 158.6 175180 0.1097 512.3 1.9256 0.8346 1.0810 159.8 0.1048 512.2 1.9230 0.8348 1.0815 159.6 180185 0.1110 516.4 1.9348 0.8387 1.0804 160.8 0.1061 516.3 1.9322 0.8389 1.0809 160.6 185190 0.1123 520.6 1.9439 0.8427 1.0798 161.8 0.1073 520.5 1.9413 0.8429 1.0803 161.6 190195 0.1136 524.9 1.9530 0.8467 1.0792 162.7 0.1086 524.8 1.9504 0.8470 1.0797 162.6 195200 0.1149 529.1 1.9620 0.8507 1.0787 163.7 0.1099 529.0 1.9594 0.8509 1.0792 163.6 200205 0.1163 533.4 1.9710 0.8547 1.0781 164.7 0.1111 533.3 1.9684 0.8549 1.0786 164.6 205

14

Page 17: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 250.00 kPa (abs)PRESSURE = 240.00 kPa (abs)

PRESSURE = 260.00 kPa (abs) PRESSURE = 270.00 kPa (abs)

53.99 0.0007 253.5 1.1777 1.0763 1.4349 595.3 SAT LIQ 0.0007 255.0 1.1822 1.0792 1.4355 590.4 55.3653.99 0.0684 412.6 1.6640 0.7678 1.1191 129.7 SAT VAP 0.0658 413.4 1.6645 0.7703 1.1200 129.7 55.36

55 0.0687 413.4 1.6664 0.7672 1.1182 130.0 — — — — — — 5560 0.0701 417.2 1.6780 0.7648 1.1143 131.5 0.0670 417.0 1.6753 0.7678 1.1161 131.1 6065 0.0714 421.0 1.6894 0.7635 1.1109 132.9 0.0683 420.8 1.6867 0.7661 1.1125 132.5 6570 0.0728 424.8 1.7006 0.7631 1.1079 134.3 0.0696 424.7 1.6980 0.7653 1.1094 133.9 7075 0.0741 428.7 1.7116 0.7635 1.1054 135.6 0.0709 428.5 1.7090 0.7654 1.1067 135.3 7580 0.0754 432.5 1.7225 0.7645 1.1031 136.9 0.0722 432.3 1.7199 0.7661 1.1043 136.6 8085 0.0767 436.3 1.7333 0.7660 1.1011 138.2 0.0734 436.1 1.7307 0.7674 1.1022 137.9 8590 0.0780 440.1 1.7439 0.7680 1.0992 139.4 0.0747 440.0 1.7414 0.7693 1.1003 139.1 9095 0.0792 444.0 1.7544 0.7704 1.0976 140.7 0.0759 443.8 1.7519 0.7715 1.0986 140.4 95

100 0.0805 447.8 1.7648 0.7731 1.0961 141.9 0.0771 447.7 1.7623 0.7741 1.0970 141.6 100105 0.0818 451.7 1.7751 0.7761 1.0948 143.1 0.0783 451.6 1.7727 0.7770 1.0956 142.8 105110 0.0830 455.6 1.7853 0.7794 1.0935 144.3 0.0795 455.5 1.7829 0.7801 1.0944 144.0 110115 0.0843 459.5 1.7955 0.7828 1.0924 145.4 0.0808 459.4 1.7930 0.7835 1.0932 145.2 115120 0.0855 463.4 1.8055 0.7864 1.0913 146.6 0.0820 463.3 1.8031 0.7870 1.0921 146.4 120125 0.0868 467.4 1.8155 0.7902 1.0903 147.7 0.0832 467.2 1.8130 0.7907 1.0910 147.5 125130 0.0880 471.3 1.8254 0.7940 1.0894 148.8 0.0844 471.2 1.8229 0.7945 1.0901 148.6 130135 0.0893 475.3 1.8352 0.7980 1.0885 150.0 0.0856 475.2 1.8327 0.7984 1.0892 149.8 135140 0.0905 479.3 1.8449 0.8020 1.0877 151.1 0.0867 479.2 1.8425 0.8024 1.0883 150.9 140145 0.0917 483.3 1.8546 0.8061 1.0869 152.2 0.0879 483.2 1.8522 0.8064 1.0875 152.0 145150 0.0930 487.4 1.8642 0.8102 1.0861 153.2 0.0891 487.3 1.8618 0.8105 1.0867 153.1 150155 0.0942 491.4 1.8737 0.8143 1.0853 154.3 0.0903 491.3 1.8713 0.8146 1.0859 154.1 155160 0.0954 495.5 1.8832 0.8185 1.0846 155.4 0.0915 495.4 1.8808 0.8187 1.0852 155.2 160165 0.0966 499.6 1.8926 0.8226 1.0839 156.4 0.0927 499.5 1.8902 0.8229 1.0845 156.3 165170 0.0979 503.7 1.9020 0.8268 1.0833 157.5 0.0938 503.6 1.8996 0.8270 1.0838 157.3 170175 0.0991 507.9 1.9113 0.8309 1.0826 158.5 0.0950 507.8 1.9089 0.8311 1.0832 158.4 175180 0.1003 512.1 1.9205 0.8350 1.0820 159.5 0.0962 511.9 1.9181 0.8353 1.0825 159.4 180185 0.1015 516.2 1.9297 0.8391 1.0814 160.5 0.0974 516.1 1.9273 0.8393 1.0819 160.4 185190 0.1028 520.4 1.9389 0.8432 1.0808 161.5 0.0986 520.3 1.9365 0.8434 1.0813 161.4 190195 0.1040 524.7 1.9479 0.8472 1.0802 162.5 0.0997 524.6 1.9455 0.8474 1.0807 162.4 195200 0.1052 528.9 1.9569 0.8512 1.0796 163.5 0.1009 528.8 1.9546 0.8514 1.0801 163.4 200205 0.1064 533.2 1.9659 0.8551 1.0791 164.5 0.1021 533.1 1.9635 0.8553 1.0795 164.4 205210 — — — — — — 0.1033 537.4 1.9724 0.8592 1.0790 165.4 210

56.69 0.0007 256.4 1.1866 1.0819 1.4362 585.6 SAT LIQ 0.0007 257.8 1.1908 1.0844 1.4368 581.0 57.9856.69 0.0634 414.2 1.6650 0.7728 1.1208 129.7 SAT VAP 0.0611 415.0 1.6654 0.7753 1.1217 129.7 57.98

60 0.0642 416.8 1.6727 0.7708 1.1180 130.7 0.0616 416.6 1.6702 0.7739 1.1199 130.3 6065 0.0655 420.6 1.6842 0.7687 1.1142 132.1 0.0629 420.4 1.6817 0.7713 1.1159 131.8 6570 0.0667 424.5 1.6954 0.7676 1.1109 133.5 0.0641 424.3 1.6930 0.7698 1.1124 133.2 7075 0.0680 428.3 1.7065 0.7673 1.1080 134.9 0.0653 428.1 1.7041 0.7693 1.1094 134.6 7580 0.0692 432.1 1.7175 0.7678 1.1055 136.3 0.0665 432.0 1.7151 0.7695 1.1068 135.9 8085 0.0704 436.0 1.7283 0.7689 1.1033 137.6 0.0676 435.8 1.7259 0.7704 1.1045 137.3 8590 0.0716 439.8 1.7389 0.7705 1.1013 138.9 0.0688 439.7 1.7366 0.7718 1.1024 138.6 9095 0.0728 443.7 1.7495 0.7726 1.0996 140.1 0.0699 443.5 1.7472 0.7737 1.1006 139.8 95

100 0.0740 447.6 1.7599 0.7751 1.0980 141.4 0.0711 447.4 1.7576 0.7760 1.0989 141.1 100105 0.0752 451.4 1.7703 0.7778 1.0965 142.6 0.0722 451.3 1.7680 0.7787 1.0974 142.3 105110 0.0763 455.3 1.7805 0.7809 1.0952 143.8 0.0734 455.2 1.7782 0.7816 1.0960 143.5 110115 0.0775 459.3 1.7906 0.7841 1.0940 145.0 0.0745 459.1 1.7884 0.7848 1.0948 144.7 115120 0.0787 463.2 1.8007 0.7876 1.0928 146.1 0.0756 463.1 1.7984 0.7882 1.0936 145.9 120125 0.0798 467.1 1.8107 0.7912 1.0918 147.3 0.0767 467.0 1.8084 0.7917 1.0925 147.1 125130 0.0810 471.1 1.8206 0.7950 1.0908 148.4 0.0779 471.0 1.8183 0.7954 1.0915 148.2 130135 0.0821 475.1 1.8304 0.7988 1.0898 149.6 0.0790 475.0 1.8281 0.7992 1.0905 149.4 135140 0.0833 479.1 1.8402 0.8028 1.0890 150.7 0.0801 479.0 1.8379 0.8031 1.0896 150.5 140145 0.0844 483.1 1.8498 0.8068 1.0881 151.8 0.0812 483.0 1.8476 0.8071 1.0888 151.6 145150 0.0856 487.1 1.8594 0.8108 1.0873 152.9 0.0823 487.0 1.8572 0.8111 1.0879 152.7 150155 0.0867 491.2 1.8690 0.8149 1.0865 154.0 0.0834 491.1 1.8667 0.8152 1.0871 153.8 155160 0.0879 495.3 1.8785 0.8190 1.0858 155.1 0.0845 495.2 1.8762 0.8193 1.0864 154.9 160165 0.0890 499.4 1.8879 0.8231 1.0851 156.1 0.0856 499.3 1.8857 0.8234 1.0856 156.0 165170 0.0901 503.5 1.8973 0.8273 1.0844 157.2 0.0867 503.4 1.8950 0.8275 1.0849 157.0 170175 0.0913 507.7 1.9066 0.8314 1.0837 158.2 0.0878 507.6 1.9043 0.8316 1.0842 158.1 175180 0.0924 511.8 1.9158 0.8355 1.0831 159.3 0.0889 511.7 1.9136 0.8357 1.0836 159.1 180185 0.0935 516.0 1.9250 0.8396 1.0824 160.3 0.0900 515.9 1.9228 0.8398 1.0829 160.2 185190 0.0947 520.2 1.9341 0.8436 1.0818 161.3 0.0911 520.1 1.9319 0.8439 1.0823 161.2 190195 0.0958 524.5 1.9432 0.8476 1.0812 162.3 0.0922 524.4 1.9410 0.8479 1.0817 162.2 195200 0.0970 528.7 1.9523 0.8516 1.0806 163.3 0.0933 528.6 1.9500 0.8519 1.0811 163.2 200205 0.0981 533.0 1.9612 0.8556 1.0800 164.3 0.0944 532.9 1.9590 0.8558 1.0805 164.2 205210 0.0992 537.3 1.9702 0.8595 1.0794 165.3 0.0955 537.2 1.9679 0.8597 1.0799 165.2 210

15

Page 18: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 300.00 kPa (abs) PRESSURE = 310.00 kPa (abs)

PRESSURE = 290.00 kPa (abs)PRESSURE = 280.00 kPa (abs)

59.24 0.0007 259.2 1.1949 1.0868 1.4375 576.5 SAT LIQ 0.0007 260.5 1.1989 1.0891 1.4382 572.1 60.4659.24 0.0590 415.8 1.6659 0.7776 1.1226 129.6 SAT VAP 0.0571 416.5 1.6664 0.7800 1.1235 129.6 60.46

60 0.0592 416.3 1.6677 0.7771 1.1219 129.9 — — — — — — 6065 0.0604 420.2 1.6792 0.7741 1.1177 131.4 0.0581 420.0 1.6769 0.7769 1.1195 131.0 6570 0.0616 424.1 1.6906 0.7722 1.1140 132.8 0.0593 423.9 1.6883 0.7746 1.1156 132.5 7075 0.0628 428.0 1.7018 0.7713 1.1109 134.2 0.0604 427.8 1.6995 0.7734 1.1123 133.9 7580 0.0639 431.8 1.7128 0.7713 1.1081 135.6 0.0615 431.6 1.7105 0.7731 1.1094 135.3 8085 0.0650 435.7 1.7236 0.7719 1.1057 137.0 0.0626 435.5 1.7214 0.7735 1.1069 136.6 8590 0.0662 439.5 1.7343 0.7731 1.1035 138.3 0.0637 439.4 1.7321 0.7745 1.1046 138.0 9095 0.0673 443.4 1.7449 0.7749 1.1016 139.6 0.0648 443.2 1.7427 0.7760 1.1026 139.3 95

100 0.0684 447.3 1.7554 0.7770 1.0999 140.8 0.0659 447.1 1.7532 0.7781 1.1008 140.6 100105 0.0695 451.2 1.7657 0.7796 1.0983 142.1 0.0670 451.0 1.7636 0.7805 1.0992 141.8 105110 0.0706 455.1 1.7760 0.7824 1.0969 143.3 0.0680 454.9 1.7738 0.7832 1.0977 143.1 110115 0.0717 459.0 1.7861 0.7855 1.0956 144.5 0.0691 458.9 1.7840 0.7862 1.0964 144.3 115120 0.0728 462.9 1.7962 0.7888 1.0944 145.7 0.0701 462.8 1.7941 0.7894 1.0951 145.5 120125 0.0739 466.9 1.8062 0.7923 1.0932 146.9 0.0712 466.8 1.8041 0.7928 1.0940 146.7 125130 0.0749 470.9 1.8161 0.7959 1.0922 148.0 0.0723 470.7 1.8140 0.7964 1.0929 147.8 130135 0.0760 474.8 1.8260 0.7997 1.0912 149.2 0.0733 474.7 1.8238 0.8001 1.0919 149.0 135140 0.0771 478.8 1.8357 0.8035 1.0903 150.3 0.0743 478.7 1.8336 0.8039 1.0909 150.1 140145 0.0782 482.9 1.8454 0.8075 1.0894 151.5 0.0754 482.8 1.8433 0.8078 1.0900 151.3 145150 0.0793 486.9 1.8550 0.8115 1.0885 152.6 0.0764 486.8 1.8529 0.8118 1.0892 152.4 150155 0.0803 491.0 1.8646 0.8155 1.0877 153.7 0.0775 490.9 1.8625 0.8158 1.0883 153.5 155160 0.0814 495.1 1.8741 0.8196 1.0870 154.8 0.0785 495.0 1.8720 0.8199 1.0876 154.6 160165 0.0824 499.2 1.8835 0.8237 1.0862 155.8 0.0795 499.1 1.8814 0.8240 1.0868 155.7 165170 0.0835 503.3 1.8929 0.8278 1.0855 156.9 0.0805 503.2 1.8908 0.8280 1.0861 156.8 170175 0.0846 507.5 1.9022 0.8319 1.0848 158.0 0.0816 507.4 1.9001 0.8321 1.0853 157.8 175180 0.0856 511.6 1.9114 0.8360 1.0841 159.0 0.0826 511.5 1.9093 0.8362 1.0846 158.9 180185 0.0867 515.8 1.9206 0.8400 1.0834 160.1 0.0836 515.7 1.9185 0.8403 1.0840 159.9 185190 0.0878 520.0 1.9298 0.8441 1.0828 161.1 0.0847 519.9 1.9277 0.8443 1.0833 161.0 190195 0.0888 524.3 1.9389 0.8481 1.0822 162.1 0.0857 524.2 1.9368 0.8483 1.0827 162.0 195200 0.0899 528.5 1.9479 0.8521 1.0815 163.1 0.0867 528.4 1.9458 0.8523 1.0820 163.0 200205 0.0909 532.8 1.9569 0.8560 1.0809 164.1 0.0877 532.7 1.9548 0.8563 1.0814 164.0 205210 0.0920 537.1 1.9658 0.8599 1.0803 165.1 0.0888 537.0 1.9637 0.8602 1.0808 165.0 210215 — — — — — — 0.0898 541.3 1.9726 0.8640 1.0802 166.0 215

61.65 0.0007 261.8 1.2027 1.0912 1.4389 567.7 SAT LIQ 0.0007 263.1 1.2065 1.0933 1.4395 563.5 62.8161.65 0.0552 417.2 1.6668 0.7822 1.1245 129.6 SAT VAP 0.0535 417.9 1.6673 0.7844 1.1254 129.5 62.81

65 0.0560 419.8 1.6746 0.7797 1.1214 130.6 0.0540 419.6 1.6724 0.7827 1.1233 130.2 6570 0.0571 423.7 1.6860 0.7771 1.1173 132.1 0.0551 423.5 1.6838 0.7796 1.1190 131.7 7075 0.0582 427.6 1.6972 0.7755 1.1138 133.5 0.0562 427.4 1.6951 0.7777 1.1153 133.2 7580 0.0593 431.5 1.7083 0.7749 1.1108 135.0 0.0572 431.3 1.7062 0.7768 1.1121 134.6 8085 0.0604 435.3 1.7192 0.7750 1.1081 136.3 0.0583 435.2 1.7171 0.7767 1.1094 136.0 8590 0.0615 439.2 1.7299 0.7759 1.1058 137.7 0.0593 439.1 1.7279 0.7773 1.1069 137.4 9095 0.0625 443.1 1.7406 0.7772 1.1037 139.0 0.0603 442.9 1.7385 0.7785 1.1047 138.7 95

100 0.0636 447.0 1.7511 0.7791 1.1018 140.3 0.0614 446.8 1.7490 0.7802 1.1028 140.0 100105 0.0646 450.9 1.7614 0.7814 1.1001 141.6 0.0624 450.8 1.7594 0.7823 1.1011 141.3 105110 0.0656 454.8 1.7717 0.7840 1.0986 142.8 0.0634 454.7 1.7697 0.7848 1.0995 142.6 110115 0.0667 458.7 1.7819 0.7869 1.0972 144.0 0.0644 458.6 1.7799 0.7876 1.0980 143.8 115120 0.0677 462.7 1.7920 0.7900 1.0959 145.3 0.0654 462.5 1.7900 0.7907 1.0967 145.0 120125 0.0687 466.6 1.8020 0.7934 1.0947 146.5 0.0664 466.5 1.8000 0.7939 1.0955 146.2 125130 0.0697 470.6 1.8119 0.7969 1.0936 147.6 0.0674 470.5 1.8099 0.7974 1.0944 147.4 130135 0.0707 474.6 1.8218 0.8006 1.0926 148.8 0.0684 474.5 1.8198 0.8010 1.0933 148.6 135140 0.0718 478.6 1.8315 0.8043 1.0916 150.0 0.0693 478.5 1.8296 0.8047 1.0923 149.8 140145 0.0728 482.6 1.8412 0.8082 1.0907 151.1 0.0703 482.5 1.8393 0.8086 1.0913 150.9 145150 0.0738 486.7 1.8509 0.8121 1.0898 152.2 0.0713 486.6 1.8489 0.8125 1.0904 152.1 150155 0.0748 490.8 1.8604 0.8161 1.0890 153.3 0.0723 490.7 1.8585 0.8165 1.0896 153.2 155160 0.0758 494.9 1.8699 0.8202 1.0882 154.5 0.0732 494.7 1.8680 0.8205 1.0888 154.3 160165 0.0768 499.0 1.8794 0.8242 1.0874 155.5 0.0742 498.9 1.8774 0.8245 1.0880 155.4 165170 0.0778 503.1 1.8887 0.8283 1.0866 156.6 0.0752 503.0 1.8868 0.8286 1.0872 156.5 170175 0.0788 507.3 1.8981 0.8324 1.0859 157.7 0.0762 507.1 1.8961 0.8326 1.0864 157.6 175180 0.0798 511.4 1.9073 0.8365 1.0852 158.8 0.0771 511.3 1.9054 0.8367 1.0857 158.6 180185 0.0808 515.6 1.9165 0.8405 1.0845 159.8 0.0781 515.5 1.9146 0.8408 1.0850 159.7 185190 0.0818 519.8 1.9257 0.8446 1.0838 160.9 0.0791 519.7 1.9237 0.8448 1.0843 160.8 190195 0.0827 524.1 1.9348 0.8486 1.0832 161.9 0.0800 524.0 1.9328 0.8488 1.0837 161.8 195200 0.0838 528.3 1.9438 0.8525 1.0825 162.9 0.0810 528.2 1.9418 0.8528 1.0830 162.8 200205 0.0847 532.6 1.9528 0.8565 1.0819 163.9 0.0819 532.5 1.9508 0.8567 1.0824 163.8 205210 0.0857 536.9 1.9617 0.8604 1.0813 164.9 0.0829 536.8 1.9598 0.8606 1.0817 164.9 210215 0.0867 541.2 1.9706 0.8642 1.0807 165.9 0.0839 541.1 1.9686 0.8645 1.0811 165.9 215

16

Page 19: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 330.00 kPa (abs)PRESSURE = 320.00 kPa (abs)

PRESSURE = 350.00 kPa (abs)PRESSURE = 340.00 kPa (abs)

63.94 0.0007 264.3 1.2102 1.0952 1.4402 559.4 SAT LIQ 0.0007 265.5 1.2137 1.0971 1.4409 555.3 65.0463.94 0.0519 418.6 1.6677 0.7866 1.1263 129.5 SAT VAP 0.0504 419.2 1.6681 0.7888 1.1273 129.4 65.04

65 0.0521 419.4 1.6702 0.7857 1.1253 129.8 — — — — — — 6570 0.0532 423.3 1.6817 0.7822 1.1208 131.4 0.0514 423.1 1.6796 0.7848 1.1226 131.0 7075 0.0542 427.2 1.6930 0.7799 1.1169 132.8 0.0524 427.0 1.6909 0.7822 1.1185 132.5 7580 0.0553 431.1 1.7041 0.7787 1.1135 134.3 0.0535 430.9 1.7020 0.7806 1.1150 134.0 8085 0.0563 435.0 1.7150 0.7783 1.1106 135.7 0.0545 434.8 1.7130 0.7800 1.1120 135.4 8590 0.0573 438.9 1.7258 0.7787 1.1081 137.1 0.0554 438.7 1.7238 0.7802 1.1093 136.8 9095 0.0583 442.8 1.7365 0.7797 1.1058 138.4 0.0564 442.6 1.7345 0.7810 1.1069 138.1 95

100 0.0593 446.7 1.7470 0.7812 1.1038 139.8 0.0574 446.6 1.7450 0.7824 1.1048 139.5 100105 0.0603 450.6 1.7574 0.7832 1.1020 141.1 0.0583 450.5 1.7555 0.7842 1.1030 140.8 105110 0.0613 454.5 1.7677 0.7856 1.1004 142.3 0.0593 454.4 1.7658 0.7865 1.1013 142.1 110115 0.0623 458.5 1.7779 0.7883 1.0989 143.6 0.0603 458.3 1.7760 0.7891 1.0997 143.3 115120 0.0632 462.4 1.7880 0.7913 1.0975 144.8 0.0612 462.3 1.7861 0.7920 1.0983 144.6 120125 0.0642 466.4 1.7980 0.7945 1.0963 146.0 0.0621 466.3 1.7961 0.7951 1.0970 145.8 125130 0.0651 470.4 1.8080 0.7979 1.0951 147.2 0.0631 470.2 1.8061 0.7984 1.0958 147.0 130135 0.0661 474.4 1.8178 0.8015 1.0940 148.4 0.0640 474.2 1.8159 0.8019 1.0947 148.2 135140 0.0671 478.4 1.8276 0.8052 1.0930 149.6 0.0649 478.3 1.8257 0.8056 1.0937 149.4 140145 0.0680 482.4 1.8373 0.8090 1.0920 150.7 0.0659 482.3 1.8354 0.8093 1.0927 150.6 145150 0.0690 486.5 1.8470 0.8128 1.0911 151.9 0.0668 486.4 1.8451 0.8132 1.0917 151.7 150155 0.0699 490.5 1.8565 0.8168 1.0902 153.0 0.0677 490.4 1.8547 0.8171 1.0908 152.9 155160 0.0709 494.6 1.8660 0.8208 1.0894 154.1 0.0686 494.5 1.8642 0.8211 1.0900 154.0 160165 0.0718 498.7 1.8755 0.8248 1.0885 155.3 0.0696 498.6 1.8736 0.8251 1.0891 155.1 165170 0.0728 502.9 1.8849 0.8289 1.0878 156.4 0.0705 502.8 1.8830 0.8291 1.0883 156.2 170175 0.0737 507.0 1.8942 0.8329 1.0870 157.4 0.0714 506.9 1.8923 0.8332 1.0876 157.3 175180 0.0746 511.2 1.9034 0.8370 1.0863 158.5 0.0723 511.1 1.9016 0.8372 1.0868 158.4 180185 0.0756 515.4 1.9127 0.8410 1.0855 159.6 0.0732 515.3 1.9108 0.8413 1.0861 159.5 185190 0.0765 519.6 1.9218 0.8450 1.0848 160.6 0.0741 519.5 1.9200 0.8453 1.0854 160.5 190195 0.0775 523.9 1.9309 0.8490 1.0842 161.7 0.0750 523.8 1.9291 0.8493 1.0847 161.6 195200 0.0784 528.1 1.9399 0.8530 1.0835 162.7 0.0759 528.0 1.9381 0.8533 1.0840 162.6 200205 0.0793 532.4 1.9489 0.8570 1.0828 163.7 0.0769 532.3 1.9471 0.8572 1.0833 163.7 205210 0.0803 536.7 1.9579 0.8609 1.0822 164.8 0.0778 536.6 1.9560 0.8611 1.0827 164.7 210215 0.0812 541.0 1.9668 0.8647 1.0816 165.8 0.0787 540.9 1.9649 0.8650 1.0820 165.7 215220 — — — — — — 0.0796 545.2 1.9738 0.8688 1.0814 166.7 220

66.12 0.0007 266.7 1.2172 1.0989 1.4416 551.4 SAT LIQ 0.0007 267.9 1.2206 1.1006 1.4423 547.5 67.1866.12 0.0489 419.9 1.6685 0.7909 1.1282 129.4 SAT VAP 0.0476 420.5 1.6690 0.7929 1.1292 129.3 67.18

70 0.0497 422.9 1.6775 0.7875 1.1244 130.6 0.0481 422.7 1.6755 0.7903 1.1263 130.2 7075 0.0507 426.8 1.6889 0.7845 1.1201 132.1 0.0491 426.7 1.6869 0.7869 1.1218 131.8 7580 0.0517 430.8 1.7001 0.7826 1.1165 133.6 0.0501 430.6 1.6981 0.7847 1.1180 133.3 8085 0.0527 434.7 1.7110 0.7817 1.1133 135.1 0.0511 434.5 1.7091 0.7835 1.1147 134.8 8590 0.0537 438.6 1.7219 0.7816 1.1105 136.5 0.0520 438.4 1.7200 0.7832 1.1118 136.2 9095 0.0546 442.5 1.7326 0.7823 1.1081 137.9 0.0529 442.3 1.7307 0.7836 1.1092 137.6 95

100 0.0556 446.4 1.7431 0.7835 1.1059 139.2 0.0539 446.3 1.7413 0.7846 1.1070 138.9 100105 0.0565 450.3 1.7536 0.7852 1.1040 140.5 0.0548 450.2 1.7517 0.7862 1.1049 140.3 105110 0.0574 454.3 1.7639 0.7873 1.1022 141.8 0.0557 454.1 1.7621 0.7882 1.1031 141.6 110115 0.0584 458.2 1.7741 0.7898 1.1006 143.1 0.0566 458.1 1.7723 0.7906 1.1015 142.9 115120 0.0593 462.2 1.7843 0.7926 1.0992 144.4 0.0575 462.0 1.7824 0.7933 1.1000 144.1 120125 0.0602 466.1 1.7943 0.7957 1.0978 145.6 0.0584 466.0 1.7925 0.7963 1.0986 145.4 125130 0.0611 470.1 1.8042 0.7990 1.0966 146.8 0.0593 470.0 1.8024 0.7995 1.0973 146.6 130135 0.0620 474.1 1.8141 0.8024 1.0954 148.0 0.0602 474.0 1.8123 0.8029 1.0962 147.8 135140 0.0629 478.1 1.8239 0.8060 1.0944 149.2 0.0610 478.0 1.8221 0.8064 1.0951 149.0 140145 0.0638 482.2 1.8336 0.8097 1.0933 150.4 0.0619 482.1 1.8318 0.8101 1.0940 150.2 145150 0.0647 486.2 1.8433 0.8135 1.0924 151.6 0.0628 486.1 1.8415 0.8139 1.0930 151.4 150155 0.0656 490.3 1.8529 0.8174 1.0914 152.7 0.0637 490.2 1.8511 0.8178 1.0921 152.5 155160 0.0665 494.4 1.8624 0.8214 1.0906 153.8 0.0646 494.3 1.8606 0.8217 1.0912 153.7 160165 0.0674 498.5 1.8718 0.8254 1.0897 155.0 0.0654 498.4 1.8700 0.8257 1.0903 154.8 165170 0.0683 502.7 1.8812 0.8294 1.0889 156.1 0.0663 502.6 1.8794 0.8297 1.0895 155.9 170175 0.0692 506.8 1.8905 0.8334 1.0881 157.2 0.0672 506.7 1.8888 0.8337 1.0887 157.0 175180 0.0701 511.0 1.8998 0.8375 1.0873 158.3 0.0680 510.9 1.8980 0.8377 1.0879 158.1 180185 0.0710 515.2 1.9090 0.8415 1.0866 159.3 0.0689 515.1 1.9073 0.8418 1.0871 159.2 185190 0.0719 519.4 1.9182 0.8455 1.0859 160.4 0.0698 519.3 1.9164 0.8458 1.0864 160.3 190195 0.0728 523.7 1.9273 0.8495 1.0852 161.5 0.0706 523.6 1.9255 0.8498 1.0857 161.4 195200 0.0736 527.9 1.9363 0.8535 1.0845 162.5 0.0715 527.8 1.9346 0.8537 1.0850 162.4 200205 0.0745 532.2 1.9453 0.8574 1.0838 163.6 0.0723 532.1 1.9436 0.8577 1.0843 163.5 205210 0.0754 536.5 1.9542 0.8613 1.0831 164.6 0.0732 536.4 1.9525 0.8616 1.0836 164.5 210215 0.0763 540.8 1.9631 0.8652 1.0825 165.6 0.0741 540.7 1.9614 0.8654 1.0830 165.5 215220 0.0772 545.1 1.9720 0.8690 1.0819 166.6 0.0749 545.0 1.9702 0.8692 1.0823 166.5 220

17

Page 20: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 380.00 kPa (abs) PRESSURE = 390.00 kPa (abs)

PRESSURE = 370.00 kPa (abs)PRESSURE = 360.00 kPa (abs)

68.21 0.0007 269.0 1.2239 1.1023 1.4430 543.7 SAT LIQ 0.0007 270.2 1.2272 1.1038 1.4437 540.0 69.2268.21 0.0463 421.1 1.6694 0.7949 1.1302 129.2 SAT VAP 0.0451 421.7 1.6698 0.7969 1.1311 129.2 69.22

70 0.0467 422.5 1.6735 0.7932 1.1283 129.8 0.0452 422.3 1.6716 0.7961 1.1303 129.4 7075 0.0476 426.5 1.6850 0.7893 1.1236 131.4 0.0462 426.3 1.6831 0.7918 1.1253 131.0 7580 0.0486 430.4 1.6962 0.7868 1.1195 132.9 0.0471 430.2 1.6943 0.7889 1.1211 132.6 8085 0.0495 434.3 1.7073 0.7853 1.1161 134.4 0.0480 434.2 1.7054 0.7871 1.1175 134.1 8590 0.0504 438.3 1.7181 0.7847 1.1130 135.9 0.0489 438.1 1.7163 0.7863 1.1143 135.6 9095 0.0513 442.2 1.7289 0.7849 1.1104 137.3 0.0498 442.0 1.7271 0.7863 1.1116 137.0 95

100 0.0522 446.1 1.7395 0.7858 1.1080 138.7 0.0507 446.0 1.7377 0.7870 1.1091 138.4 100105 0.0531 450.0 1.7499 0.7872 1.1059 140.0 0.0516 449.9 1.7482 0.7883 1.1070 139.7 105110 0.0540 454.0 1.7603 0.7891 1.1041 141.3 0.0525 453.8 1.7585 0.7900 1.1050 141.1 110115 0.0549 457.9 1.7705 0.7914 1.1024 142.6 0.0533 457.8 1.7688 0.7922 1.1033 142.4 115120 0.0558 461.9 1.7807 0.7940 1.1008 143.9 0.0542 461.8 1.7789 0.7947 1.1017 143.7 120125 0.0567 465.9 1.7907 0.7969 1.0994 145.2 0.0550 465.8 1.7890 0.7975 1.1002 144.9 125130 0.0575 469.9 1.8007 0.8000 1.0981 146.4 0.0559 469.7 1.7990 0.8006 1.0989 146.2 130135 0.0584 473.9 1.8106 0.8034 1.0969 147.6 0.0567 473.8 1.8089 0.8039 1.0976 147.4 135140 0.0592 477.9 1.8204 0.8069 1.0958 148.8 0.0576 477.8 1.8187 0.8073 1.0965 148.7 140145 0.0601 481.9 1.8301 0.8105 1.0947 150.0 0.0584 481.8 1.8284 0.8109 1.0954 149.9 145150 0.0610 486.0 1.8398 0.8143 1.0937 151.2 0.0592 485.9 1.8381 0.8146 1.0943 151.0 150155 0.0618 490.1 1.8493 0.8181 1.0927 152.4 0.0601 490.0 1.8477 0.8185 1.0934 152.2 155160 0.0627 494.2 1.8589 0.8220 1.0918 153.5 0.0609 494.1 1.8572 0.8223 1.0924 153.4 160165 0.0635 498.3 1.8683 0.8260 1.0909 154.7 0.0617 498.2 1.8666 0.8263 1.0915 154.5 165170 0.0644 502.5 1.8777 0.8300 1.0901 155.8 0.0626 502.3 1.8760 0.8302 1.0906 155.6 170175 0.0652 506.6 1.8871 0.8340 1.0892 156.9 0.0634 506.5 1.8854 0.8342 1.0898 156.8 175180 0.0661 510.8 1.8963 0.8380 1.0884 158.0 0.0642 510.7 1.8947 0.8382 1.0890 157.9 180185 0.0669 515.0 1.9055 0.8420 1.0877 159.1 0.0650 514.9 1.9039 0.8423 1.0882 159.0 185190 0.0678 519.2 1.9147 0.8460 1.0869 160.2 0.0659 519.1 1.9130 0.8463 1.0875 160.1 190195 0.0686 523.5 1.9238 0.8500 1.0862 161.3 0.0667 523.3 1.9221 0.8502 1.0867 161.1 195200 0.0694 527.7 1.9329 0.8540 1.0855 162.3 0.0675 527.6 1.9312 0.8542 1.0860 162.2 200205 0.0703 532.0 1.9419 0.8579 1.0848 163.4 0.0683 531.9 1.9402 0.8582 1.0853 163.3 205210 0.0711 536.3 1.9508 0.8618 1.0841 164.4 0.0691 536.2 1.9491 0.8621 1.0846 164.3 210215 0.0720 540.6 1.9597 0.8657 1.0834 165.4 0.0700 540.5 1.9580 0.8659 1.0839 165.3 215220 0.0728 544.9 1.9685 0.8695 1.0828 166.5 0.0708 544.9 1.9669 0.8697 1.0832 166.4 220

70.22 0.0007 271.3 1.2304 1.1054 1.4444 536.3 SAT LIQ 0.0007 272.3 1.2335 1.1068 1.4451 532.7 71.1970.22 0.0439 422.3 1.6702 0.7989 1.1321 129.1 SAT VAP 0.0428 422.8 1.6706 0.8008 1.1331 129.0 71.19

75 0.0448 426.1 1.6812 0.7944 1.1272 130.7 0.0435 425.9 1.6794 0.7970 1.1290 130.3 7580 0.0457 430.0 1.6925 0.7911 1.1227 132.2 0.0444 429.9 1.6907 0.7933 1.1244 131.9 8085 0.0466 434.0 1.7036 0.7890 1.1189 133.8 0.0453 433.8 1.7018 0.7909 1.1204 133.4 8590 0.0475 437.9 1.7145 0.7879 1.1156 135.3 0.0462 437.8 1.7128 0.7896 1.1170 134.9 9095 0.0484 441.9 1.7253 0.7877 1.1128 136.7 0.0470 441.7 1.7236 0.7891 1.1140 136.4 95

100 0.0493 445.8 1.7359 0.7882 1.1102 138.1 0.0479 445.7 1.7342 0.7894 1.1114 137.8 100105 0.0501 449.8 1.7464 0.7893 1.1080 139.5 0.0487 449.6 1.7448 0.7904 1.1091 139.2 105110 0.0510 453.7 1.7568 0.7909 1.1060 140.8 0.0496 453.6 1.7551 0.7919 1.1070 140.6 110115 0.0518 457.7 1.7671 0.7930 1.1042 142.2 0.0504 457.5 1.7654 0.7938 1.1051 141.9 115120 0.0526 461.6 1.7773 0.7954 1.1025 143.5 0.0512 461.5 1.7756 0.7961 1.1034 143.2 120125 0.0535 465.6 1.7873 0.7982 1.1010 144.7 0.0520 465.5 1.7857 0.7988 1.1019 144.5 125130 0.0543 469.6 1.7973 0.8012 1.0997 146.0 0.0528 469.5 1.7957 0.8017 1.1005 145.8 130135 0.0551 473.6 1.8072 0.8044 1.0984 147.2 0.0536 473.5 1.8056 0.8049 1.0991 147.0 135140 0.0560 477.7 1.8170 0.8078 1.0972 148.5 0.0544 477.5 1.8154 0.8082 1.0979 148.3 140145 0.0568 481.7 1.8267 0.8113 1.0961 149.7 0.0552 481.6 1.8251 0.8118 1.0968 149.5 145150 0.0576 485.8 1.8364 0.8150 1.0950 150.9 0.0560 485.7 1.8348 0.8154 1.0957 150.7 150155 0.0584 489.9 1.8460 0.8188 1.0940 152.0 0.0568 489.8 1.8444 0.8192 1.0946 151.9 155160 0.0592 494.0 1.8555 0.8227 1.0930 153.2 0.0576 493.9 1.8539 0.8230 1.0937 153.1 160165 0.0600 498.1 1.8650 0.8266 1.0921 154.4 0.0584 498.0 1.8634 0.8269 1.0927 154.2 165170 0.0608 502.2 1.8744 0.8305 1.0912 155.5 0.0592 502.1 1.8728 0.8308 1.0918 155.4 170175 0.0617 506.4 1.8837 0.8345 1.0904 156.6 0.0600 506.3 1.8822 0.8348 1.0910 156.5 175180 0.0625 510.6 1.8930 0.8385 1.0896 157.8 0.0608 510.5 1.8914 0.8388 1.0901 157.6 180185 0.0633 514.8 1.9022 0.8425 1.0888 158.9 0.0616 514.7 1.9007 0.8428 1.0893 158.7 185190 0.0641 519.0 1.9114 0.8465 1.0880 159.9 0.0624 518.9 1.9098 0.8468 1.0885 159.8 190195 0.0649 523.2 1.9205 0.8505 1.0872 161.0 0.0632 523.1 1.9189 0.8507 1.0877 160.9 195200 0.0657 527.5 1.9296 0.8545 1.0865 162.1 0.0639 527.4 1.9280 0.8547 1.0870 162.0 200205 0.0665 531.8 1.9386 0.8584 1.0858 163.2 0.0647 531.7 1.9370 0.8586 1.0862 163.1 205210 0.0673 536.1 1.9475 0.8623 1.0850 164.2 0.0655 536.0 1.9460 0.8625 1.0855 164.1 210215 0.0681 540.4 1.9564 0.8662 1.0843 165.3 0.0663 540.3 1.9549 0.8664 1.0848 165.2 215220 0.0689 544.8 1.9653 0.8700 1.0837 166.3 0.0671 544.7 1.9637 0.8702 1.0841 166.2 220225 0.0697 549.1 1.9741 0.8737 1.0830 167.3 0.0678 549.0 1.9725 0.8740 1.0834 167.2 225

18

Page 21: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 425.00 kPa (abs)PRESSURE = 400.00 kPa (abs)

PRESSURE = 450.00 kPa (abs) PRESSURE = 475.00 kPa (abs)

72.14 0.0007 273.4 1.2365 1.1082 1.4458 529.1 SAT LIQ 0.0008 276.0 1.2439 1.1116 1.4475 520.5 74.4572.14 0.0418 423.4 1.6710 0.8028 1.1341 129.0 SAT VAP 0.0394 424.7 1.6719 0.8074 1.1367 128.8 74.45

75 0.0423 425.7 1.6776 0.7997 1.1310 129.9 0.0395 425.2 1.6732 0.8068 1.1360 129.0 7580 0.0432 429.7 1.6889 0.7956 1.1261 131.5 0.0403 429.2 1.6847 0.8016 1.1306 130.6 8085 0.0441 433.6 1.7001 0.7929 1.1220 133.1 0.0412 433.2 1.6959 0.7980 1.1259 132.3 8590 0.0449 437.6 1.7111 0.7913 1.1184 134.6 0.0420 437.2 1.7069 0.7957 1.1219 133.8 9095 0.0457 441.6 1.7219 0.7906 1.1153 136.1 0.0428 441.2 1.7178 0.7944 1.1185 135.4 95

100 0.0466 445.5 1.7326 0.7907 1.1125 137.5 0.0436 445.1 1.7285 0.7940 1.1155 136.8 100105 0.0474 449.5 1.7431 0.7915 1.1101 138.9 0.0444 449.1 1.7391 0.7943 1.1129 138.3 105110 0.0482 453.4 1.7535 0.7928 1.1080 140.3 0.0451 453.1 1.7495 0.7953 1.1105 139.7 110115 0.0490 457.4 1.7638 0.7947 1.1060 141.7 0.0459 457.1 1.7599 0.7968 1.1084 141.1 115120 0.0498 461.4 1.7740 0.7969 1.1043 143.0 0.0467 461.0 1.7701 0.7988 1.1066 142.4 120125 0.0506 465.4 1.7841 0.7995 1.1027 144.3 0.0474 465.0 1.7802 0.8011 1.1048 143.7 125130 0.0514 469.4 1.7941 0.8023 1.1013 145.6 0.0482 469.1 1.7902 0.8038 1.1033 145.0 130135 0.0522 473.4 1.8040 0.8054 1.0999 146.8 0.0489 473.1 1.8001 0.8067 1.1018 146.3 135140 0.0530 477.4 1.8138 0.8087 1.0986 148.1 0.0497 477.1 1.8100 0.8099 1.1005 147.6 140145 0.0538 481.5 1.8235 0.8122 1.0975 149.3 0.0504 481.2 1.8197 0.8133 1.0992 148.8 145150 0.0546 485.5 1.8332 0.8158 1.0964 150.5 0.0512 485.3 1.8294 0.8168 1.0981 150.1 150155 0.0553 489.6 1.8428 0.8195 1.0953 151.7 0.0519 489.4 1.8390 0.8204 1.0970 151.3 155160 0.0561 493.7 1.8524 0.8233 1.0943 152.9 0.0527 493.5 1.8486 0.8242 1.0959 152.5 160165 0.0569 497.9 1.8618 0.8272 1.0933 154.1 0.0534 497.6 1.8581 0.8280 1.0949 153.7 165170 0.0577 502.0 1.8712 0.8311 1.0924 155.2 0.0541 501.7 1.8675 0.8319 1.0939 154.9 170175 0.0585 506.2 1.8806 0.8351 1.0915 156.4 0.0549 505.9 1.8768 0.8358 1.0930 156.0 175180 0.0592 510.4 1.8899 0.8390 1.0907 157.5 0.0556 510.1 1.8861 0.8397 1.0921 157.2 180185 0.0600 514.6 1.8991 0.8430 1.0898 158.6 0.0563 514.3 1.8954 0.8437 1.0912 158.3 185190 0.0608 518.8 1.9083 0.8470 1.0890 159.7 0.0571 518.5 1.9045 0.8477 1.0904 159.4 190195 0.0615 523.0 1.9174 0.8510 1.0883 160.8 0.0578 522.8 1.9137 0.8516 1.0896 160.5 195200 0.0623 527.3 1.9265 0.8549 1.0875 161.9 0.0585 527.1 1.9227 0.8556 1.0888 161.6 200205 0.0631 531.6 1.9355 0.8589 1.0867 163.0 0.0592 531.3 1.9317 0.8595 1.0880 162.7 205210 0.0638 535.9 1.9444 0.8628 1.0860 164.0 0.0600 535.7 1.9407 0.8634 1.0872 163.8 210215 0.0646 540.2 1.9533 0.8666 1.0853 165.1 0.0607 540.0 1.9496 0.8673 1.0864 164.9 215220 0.0653 544.6 1.9622 0.8705 1.0846 166.1 0.0614 544.3 1.9585 0.8711 1.0857 165.9 220225 0.0661 548.9 1.9710 0.8742 1.0839 167.2 0.0621 548.7 1.9673 0.8749 1.0850 167.0 225

76.66 0.0008 278.4 1.2509 1.1147 1.4493 512.3 SAT LIQ 0.0008 280.8 1.2576 1.1176 1.4511 504.3 78.7776.66 0.0372 426.0 1.6728 0.8120 1.1393 128.6 SAT VAP 0.0353 427.2 1.6737 0.8164 1.1420 128.4 78.77

80 0.0378 428.7 1.6805 0.8080 1.1353 129.7 0.0355 428.2 1.6765 0.8148 1.1404 128.8 8085 0.0386 432.8 1.6919 0.8034 1.1301 131.4 0.0363 432.3 1.6880 0.8092 1.1346 130.5 8590 0.0394 436.8 1.7030 0.8003 1.1257 133.0 0.0370 436.3 1.6992 0.8052 1.1297 132.2 9095 0.0401 440.8 1.7139 0.7984 1.1219 134.6 0.0378 440.3 1.7101 0.8026 1.1255 133.8 95

100 0.0409 444.7 1.7247 0.7974 1.1186 136.1 0.0385 444.4 1.7210 0.8011 1.1219 135.4 100105 0.0417 448.7 1.7353 0.7973 1.1157 137.6 0.0392 448.4 1.7316 0.8005 1.1187 136.9 105110 0.0424 452.7 1.7458 0.7979 1.1132 139.0 0.0399 452.4 1.7421 0.8006 1.1159 138.4 110115 0.0431 456.7 1.7561 0.7991 1.1109 140.4 0.0407 456.4 1.7525 0.8015 1.1135 139.8 115120 0.0439 460.7 1.7663 0.8008 1.1089 141.8 0.0414 460.4 1.7628 0.8029 1.1113 141.2 120125 0.0446 464.7 1.7765 0.8029 1.1070 143.2 0.0420 464.4 1.7729 0.8047 1.1093 142.6 125130 0.0453 468.7 1.7865 0.8054 1.1053 144.5 0.0427 468.4 1.7830 0.8070 1.1075 144.0 130135 0.0460 472.8 1.7965 0.8081 1.1038 145.8 0.0434 472.5 1.7930 0.8096 1.1058 145.3 135140 0.0467 476.8 1.8063 0.8112 1.1024 147.1 0.0441 476.5 1.8028 0.8124 1.1043 146.6 140145 0.0475 480.9 1.8161 0.8144 1.1010 148.4 0.0448 480.6 1.8126 0.8156 1.1029 147.9 145150 0.0482 485.0 1.8258 0.8178 1.0998 149.6 0.0455 484.7 1.8223 0.8189 1.1016 149.2 150155 0.0489 489.1 1.8354 0.8214 1.0986 150.9 0.0461 488.8 1.8320 0.8223 1.1003 150.5 155160 0.0496 493.2 1.8450 0.8250 1.0975 152.1 0.0468 492.9 1.8415 0.8259 1.0992 151.7 160165 0.0503 497.3 1.8545 0.8288 1.0965 153.3 0.0475 497.0 1.8510 0.8296 1.0981 152.9 165170 0.0510 501.5 1.8639 0.8326 1.0954 154.5 0.0481 501.2 1.8605 0.8334 1.0970 154.1 170175 0.0517 505.6 1.8733 0.8365 1.0945 155.7 0.0488 505.4 1.8699 0.8372 1.0960 155.3 175180 0.0524 509.8 1.8826 0.8404 1.0935 156.8 0.0495 509.6 1.8792 0.8411 1.0950 156.5 180185 0.0531 514.0 1.8918 0.8444 1.0926 158.0 0.0501 513.8 1.8884 0.8450 1.0940 157.7 185190 0.0537 518.3 1.9010 0.8483 1.0917 159.1 0.0508 518.0 1.8976 0.8490 1.0931 158.8 190195 0.0544 522.5 1.9101 0.8523 1.0909 160.3 0.0515 522.3 1.9067 0.8529 1.0922 160.0 195200 0.0551 526.8 1.9192 0.8562 1.0900 161.4 0.0521 526.5 1.9158 0.8568 1.0913 161.1 200205 0.0558 531.1 1.9282 0.8601 1.0892 162.5 0.0528 530.8 1.9249 0.8608 1.0905 162.2 205210 0.0565 535.4 1.9372 0.8640 1.0884 163.6 0.0534 535.2 1.9338 0.8646 1.0896 163.3 210215 0.0572 539.7 1.9461 0.8679 1.0876 164.6 0.0541 539.5 1.9428 0.8685 1.0888 164.4 215220 0.0579 544.1 1.9550 0.8717 1.0869 165.7 0.0547 543.8 1.9516 0.8723 1.0880 165.5 220225 0.0586 548.5 1.9638 0.8755 1.0861 166.8 0.0554 548.2 1.9604 0.8761 1.0872 166.6 225230 0.0593 552.8 1.9725 0.8792 1.0854 167.8 0.0560 552.6 1.9692 0.8799 1.0865 167.6 230

19

Page 22: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 525.00 kPa (abs)PRESSURE = 500.00 kPa (abs)

PRESSURE = 575.00 kPa (abs)PRESSURE = 550.00 kPa (abs)

80.81 0.0008 283.1 1.2640 1.1204 1.4529 496.7 SAT LIQ 0.0008 285.3 1.2701 1.1230 1.4547 489.3 82.7780.81 0.0336 428.4 1.6746 0.8208 1.1447 128.1 SAT VAP 0.0320 429.5 1.6754 0.8251 1.1475 127.9 82.77

85 0.0342 431.8 1.6842 0.8153 1.1394 129.6 0.0323 431.3 1.6805 0.8218 1.1445 128.7 8590 0.0349 435.9 1.6955 0.8104 1.1339 131.4 0.0330 435.4 1.6919 0.8159 1.1384 130.5 9095 0.0356 439.9 1.7065 0.8070 1.1292 133.0 0.0337 439.5 1.7030 0.8117 1.1332 132.2 95

100 0.0363 444.0 1.7174 0.8049 1.1253 134.6 0.0344 443.6 1.7139 0.8089 1.1288 133.9 100105 0.0370 448.0 1.7281 0.8037 1.1218 136.2 0.0351 447.6 1.7247 0.8072 1.1250 135.5 105110 0.0377 452.0 1.7386 0.8035 1.1188 137.7 0.0357 451.6 1.7353 0.8065 1.1217 137.0 110115 0.0384 456.0 1.7491 0.8039 1.1161 139.2 0.0364 455.7 1.7457 0.8065 1.1188 138.5 115120 0.0391 460.0 1.7594 0.8050 1.1137 140.6 0.0370 459.7 1.7561 0.8073 1.1163 140.0 120125 0.0398 464.1 1.7695 0.8066 1.1116 142.0 0.0377 463.7 1.7663 0.8086 1.1140 141.5 125130 0.0404 468.1 1.7796 0.8087 1.1097 143.4 0.0383 467.8 1.7764 0.8104 1.1119 142.9 130135 0.0411 472.2 1.7896 0.8111 1.1079 144.8 0.0390 471.8 1.7864 0.8126 1.1100 144.3 135140 0.0417 476.2 1.7995 0.8138 1.1063 146.1 0.0396 475.9 1.7963 0.8152 1.1083 145.6 140145 0.0424 480.3 1.8093 0.8168 1.1048 147.5 0.0402 480.0 1.8061 0.8180 1.1067 147.0 145150 0.0430 484.4 1.8190 0.8200 1.1034 148.8 0.0408 484.1 1.8159 0.8211 1.1052 148.3 150155 0.0437 488.5 1.8287 0.8233 1.1021 150.0 0.0415 488.2 1.8255 0.8244 1.1038 149.6 155160 0.0443 492.6 1.8383 0.8268 1.1008 151.3 0.0421 492.3 1.8351 0.8278 1.1025 150.9 160165 0.0450 496.8 1.8478 0.8305 1.0997 152.5 0.0427 496.5 1.8446 0.8314 1.1013 152.2 165170 0.0456 500.9 1.8572 0.8342 1.0986 153.8 0.0433 500.6 1.8541 0.8350 1.1001 153.4 170175 0.0462 505.1 1.8666 0.8380 1.0975 155.0 0.0439 504.8 1.8635 0.8388 1.0990 154.6 175180 0.0469 509.3 1.8759 0.8418 1.0964 156.2 0.0445 509.0 1.8728 0.8426 1.0979 155.8 180185 0.0475 513.5 1.8852 0.8457 1.0954 157.4 0.0451 513.3 1.8821 0.8464 1.0969 157.0 185190 0.0481 517.8 1.8944 0.8496 1.0945 158.5 0.0457 517.5 1.8913 0.8503 1.0959 158.2 190195 0.0488 522.0 1.9035 0.8536 1.0935 159.7 0.0463 521.8 1.9004 0.8542 1.0949 159.4 195200 0.0494 526.3 1.9126 0.8575 1.0926 160.8 0.0469 526.0 1.9095 0.8581 1.0940 160.6 200205 0.0500 530.6 1.9216 0.8614 1.0917 162.0 0.0476 530.3 1.9186 0.8620 1.0930 161.7 205210 0.0507 534.9 1.9306 0.8653 1.0909 163.1 0.0482 534.7 1.9276 0.8659 1.0921 162.8 210215 0.0513 539.2 1.9396 0.8691 1.0900 164.2 0.0488 539.0 1.9365 0.8698 1.0912 164.0 215220 0.0519 543.6 1.9484 0.8730 1.0892 165.3 0.0494 543.4 1.9454 0.8736 1.0904 165.1 220225 0.0525 548.0 1.9573 0.8768 1.0884 166.4 0.0500 547.7 1.9542 0.8774 1.0895 166.2 225230 0.0532 552.4 1.9660 0.8805 1.0876 167.4 0.0505 552.1 1.9630 0.8812 1.0887 167.3 230235 0.0538 556.8 1.9748 0.8842 1.0868 168.5 0.05131 556.5 1.9717 0.8849 1.0879 168.3 235

84.66 0.0008 287.4 1.2760 1.1256 1.4565 482.1 SAT LIQ 0.0008 289.5 1.2817 1.1280 1.4583 475.2 86.4984.66 0.0305 430.6 1.6762 0.8293 1.1504 127.7 SAT VAP 0.0292 431.6 1.6769 0.8335 1.1533 127.4 86.49

85 0.0306 430.9 1.6770 0.8288 1.1499 127.8 — — — — — — 8590 0.0313 435.0 1.6884 0.8218 1.1431 129.6 0.0297 434.5 1.6850 0.8280 1.1481 128.8 9095 0.0320 439.1 1.6996 0.8167 1.1374 131.4 0.0303 438.6 1.6963 0.8219 1.1418 130.6 95

100 0.0326 443.1 1.7106 0.8131 1.1326 133.1 0.0310 442.7 1.7073 0.8176 1.1365 132.3 100105 0.0333 447.2 1.7214 0.8108 1.1284 134.8 0.0316 446.8 1.7182 0.8147 1.1319 134.0 105110 0.0339 451.3 1.7320 0.8096 1.1248 136.4 0.0322 450.9 1.7289 0.8129 1.1280 135.7 110115 0.0345 455.3 1.7425 0.8093 1.1217 137.9 0.0329 454.9 1.7394 0.8121 1.1246 137.3 115120 0.0352 459.3 1.7529 0.8097 1.1189 139.4 0.0335 459.0 1.7498 0.8121 1.1216 138.8 120125 0.0358 463.4 1.7631 0.8107 1.1164 140.9 0.0341 463.1 1.7601 0.8128 1.1189 140.3 125130 0.0364 467.5 1.7733 0.8122 1.1142 142.3 0.0347 467.1 1.7702 0.8141 1.1166 141.8 130135 0.0370 471.5 1.7833 0.8142 1.1122 143.8 0.0353 471.2 1.7803 0.8159 1.1144 143.2 135140 0.0376 475.6 1.7932 0.8166 1.1104 145.1 0.0358 475.3 1.7902 0.8181 1.1125 144.6 140145 0.0382 479.7 1.8031 0.8193 1.1087 146.5 0.0364 479.4 1.8001 0.8206 1.1107 146.0 145150 0.0388 483.8 1.8128 0.8222 1.1071 147.9 0.0370 483.5 1.8099 0.8235 1.1090 147.4 150155 0.0394 487.9 1.8225 0.8254 1.1056 149.2 0.0376 487.6 1.8196 0.8265 1.1075 148.7 155160 0.0400 492.0 1.8321 0.8288 1.1043 150.5 0.0382 491.8 1.8292 0.8298 1.1060 150.1 160165 0.0406 496.2 1.8416 0.8323 1.1030 151.8 0.0387 495.9 1.8387 0.8332 1.1047 151.4 165170 0.0412 500.4 1.8511 0.8359 1.1017 153.0 0.0393 500.1 1.8482 0.8367 1.1034 152.7 170175 0.0418 504.6 1.8605 0.8396 1.1006 154.3 0.0399 504.3 1.8576 0.8404 1.1021 153.9 175180 0.0424 508.8 1.8698 0.8433 1.0994 155.5 0.0404 508.5 1.8669 0.8441 1.1010 155.2 180185 0.0430 513.0 1.8791 0.8472 1.0983 156.7 0.0410 512.7 1.8762 0.8479 1.0998 156.4 185190 0.0436 517.2 1.8883 0.8510 1.0973 157.9 0.0416 517.0 1.8855 0.8517 1.0987 157.6 190195 0.0441 521.5 1.8975 0.8549 1.0963 159.1 0.0421 521.2 1.8946 0.8556 1.0977 158.8 195200 0.0447 525.8 1.9066 0.8588 1.0953 160.3 0.0427 525.5 1.9037 0.8595 1.0966 160.0 200205 0.0453 530.1 1.9156 0.8627 1.0943 161.5 0.0432 529.8 1.9128 0.8634 1.0956 161.2 205210 0.0459 534.4 1.9246 0.8666 1.0934 162.6 0.0438 534.2 1.9218 0.8672 1.0947 162.4 210215 0.0465 538.8 1.9336 0.8704 1.0925 163.7 0.0444 538.5 1.9307 0.8711 1.0937 163.5 215220 0.0470 543.1 1.9425 0.8743 1.0916 164.9 0.0449 542.9 1.9396 0.8749 1.0928 164.6 220225 0.0476 547.5 1.9513 0.8781 1.0907 166.0 0.0455 547.3 1.9485 0.8787 1.0918 165.8 225230 0.0482 551.9 1.9601 0.8818 1.0898 167.1 0.0460 551.7 1.9573 0.8825 1.0910 166.9 230235 0.0487 556.3 1.9688 0.8855 1.0890 168.1 0.0466 556.1 1.9660 0.8862 1.0901 168.0 235240 — — — — — — 0.0471 560.5 1.9747 0.8898 1.0892 169.1 240

20

Page 23: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 625.00 kPa (abs)PRESSURE = 600.00 kPa (abs)

PRESSURE = 650.00 kPa (abs) PRESSURE = 675.00 kPa (abs)

88.26 0.0008 291.5 1.2872 1.1304 1.4602 468.5 SAT LIQ 0.0008 293.4 1.2925 1.1327 1.4621 462.0 89.9888.26 0.0280 432.6 1.6777 0.8376 1.1563 127.2 SAT VAP 0.0269 433.5 1.6784 0.8417 1.1593 126.9 89.98

90 0.0282 434.0 1.6817 0.8346 1.1535 127.8 0.0269 433.5 1.6785 0.8417 1.1593 126.9 9095 0.0289 438.2 1.6931 0.8275 1.1465 129.7 0.0275 437.7 1.6899 0.8334 1.1515 128.9 95

100 0.0295 442.3 1.7042 0.8223 1.1406 131.5 0.0281 441.9 1.7011 0.8273 1.1450 130.7 100105 0.0301 446.4 1.7151 0.8187 1.1356 133.3 0.0287 446.0 1.7121 0.8229 1.1395 132.5 105110 0.0307 450.5 1.7258 0.8164 1.1314 135.0 0.0293 450.1 1.7229 0.8200 1.1349 134.3 110115 0.0313 454.6 1.7364 0.8151 1.1277 136.6 0.0299 454.2 1.7335 0.8182 1.1308 135.9 115120 0.0319 458.6 1.7469 0.8147 1.1244 138.2 0.0305 458.3 1.7440 0.8174 1.1273 137.5 120125 0.0325 462.7 1.7571 0.8151 1.1216 139.7 0.0310 462.4 1.7543 0.8175 1.1242 139.1 125130 0.0331 466.8 1.7673 0.8161 1.1190 141.2 0.0316 466.5 1.7645 0.8182 1.1215 140.6 130135 0.0336 470.9 1.7774 0.8177 1.1167 142.7 0.0321 470.6 1.7746 0.8195 1.1191 142.1 135140 0.0342 475.0 1.7874 0.8197 1.1146 144.1 0.0327 474.7 1.7846 0.8213 1.1168 143.6 140145 0.0348 479.1 1.7972 0.8220 1.1127 145.5 0.0332 478.8 1.7945 0.8235 1.1148 145.1 145150 0.0353 483.2 1.8070 0.8247 1.1110 146.9 0.0338 482.9 1.8043 0.8260 1.1129 146.5 150155 0.0359 487.3 1.8167 0.8276 1.1093 148.3 0.0343 487.0 1.8140 0.8288 1.1112 147.9 155160 0.0364 491.5 1.8264 0.8308 1.1078 149.6 0.0349 491.2 1.8236 0.8319 1.1096 149.2 160165 0.0370 495.6 1.8359 0.8341 1.1064 151.0 0.0354 495.4 1.8332 0.8351 1.1081 150.6 165170 0.0375 499.8 1.8454 0.8376 1.1050 152.3 0.0359 499.5 1.8427 0.8385 1.1067 151.9 170175 0.0381 504.0 1.8548 0.8412 1.1037 153.6 0.0365 503.7 1.8521 0.8421 1.1053 153.2 175180 0.0386 508.2 1.8642 0.8449 1.1025 154.8 0.0370 508.0 1.8615 0.8457 1.1041 154.5 180185 0.0392 512.5 1.8735 0.8487 1.1013 156.1 0.0375 512.2 1.8708 0.8494 1.1028 155.8 185190 0.0397 516.7 1.8827 0.8525 1.1002 157.3 0.0380 516.5 1.8800 0.8532 1.1016 157.0 190195 0.0403 521.0 1.8919 0.8563 1.0991 158.5 0.0386 520.7 1.8892 0.8570 1.1005 158.2 195200 0.0408 525.3 1.9010 0.8602 1.0980 159.7 0.0391 525.0 1.8983 0.8609 1.0994 159.5 200205 0.0414 529.6 1.9100 0.8640 1.0969 160.9 0.0396 529.3 1.9074 0.8647 1.0983 160.7 205210 0.0419 533.9 1.9190 0.8679 1.0959 162.1 0.0401 533.7 1.9164 0.8686 1.0972 161.9 210215 0.0424 538.3 1.9280 0.8718 1.0949 163.3 0.0406 538.0 1.9254 0.8724 1.0962 163.0 215220 0.0430 542.6 1.9369 0.8756 1.0940 164.4 0.0412 542.4 1.9343 0.8762 1.0952 164.2 220225 0.0435 547.0 1.9458 0.8794 1.0930 165.6 0.0417 546.8 1.9431 0.8800 1.0942 165.3 225230 0.0440 551.4 1.9546 0.8831 1.0921 166.7 0.0422 551.2 1.9520 0.8838 1.0932 166.5 230235 0.0446 555.9 1.9633 0.8868 1.0912 167.8 0.0427 555.6 1.9607 0.8875 1.0923 167.6 235240 0.0451 560.3 1.9720 0.8905 1.0903 168.9 0.0432 560.1 1.9694 0.8912 1.0914 168.7 240

91.64 0.0008 295.3 1.2977 1.1350 1.4640 455.7 SAT LIQ 0.0008 297.1 1.3026 1.1373 1.4660 449.6 93.2691.64 0.0258 434.4 1.6791 0.8458 1.1624 126.7 SAT VAP 0.0249 435.3 1.6798 0.8499 1.1655 126.4 93.26

95 0.0262 437.3 1.6868 0.8397 1.1568 128.0 0.0251 436.8 1.6838 0.8464 1.1624 127.1 95100 0.0268 441.4 1.6981 0.8326 1.1496 129.9 0.0257 441.0 1.6951 0.8382 1.1545 129.1 100105 0.0274 445.6 1.7091 0.8274 1.1436 131.8 0.0262 445.2 1.7062 0.8321 1.1479 131.0 105110 0.0280 449.7 1.7200 0.8238 1.1385 133.5 0.0268 449.3 1.7172 0.8278 1.1423 132.8 110115 0.0286 453.8 1.7306 0.8215 1.1341 135.2 0.0274 453.4 1.7279 0.8249 1.1376 134.6 115120 0.0291 457.9 1.7411 0.8203 1.1303 136.9 0.0279 457.6 1.7384 0.8232 1.1335 136.3 120125 0.0297 462.0 1.7515 0.8199 1.1270 138.5 0.0284 461.7 1.7488 0.8225 1.1299 137.9 125130 0.0302 466.1 1.7617 0.8203 1.1241 140.1 0.0290 465.8 1.7591 0.8226 1.1267 139.5 130135 0.0308 470.2 1.7719 0.8214 1.1215 141.6 0.0295 469.9 1.7692 0.8233 1.1239 141.1 135140 0.0313 474.3 1.7819 0.8229 1.1191 143.1 0.0300 474.0 1.7793 0.8247 1.1214 142.6 140145 0.0318 478.5 1.7918 0.8249 1.1170 144.6 0.0305 478.2 1.7892 0.8265 1.1191 144.1 145150 0.0324 482.6 1.8016 0.8273 1.1150 146.0 0.0310 482.3 1.7990 0.8287 1.1171 145.5 150155 0.0329 486.7 1.8113 0.8300 1.1132 147.4 0.0316 486.4 1.8088 0.8313 1.1151 147.0 155160 0.0334 490.9 1.8210 0.8330 1.1115 148.8 0.0321 490.6 1.8184 0.8341 1.1134 148.4 160165 0.0339 495.1 1.8306 0.8361 1.1099 150.2 0.0326 494.8 1.8280 0.8372 1.1117 149.8 165170 0.0344 499.3 1.8401 0.8395 1.1084 151.5 0.0331 499.0 1.8375 0.8404 1.1101 151.1 170175 0.0350 503.5 1.8495 0.8430 1.1070 152.8 0.0336 503.2 1.8470 0.8439 1.1086 152.5 175180 0.0355 507.7 1.8589 0.8465 1.1056 154.1 0.0341 507.4 1.8564 0.8474 1.1072 153.8 180185 0.0360 511.9 1.8682 0.8502 1.1043 155.4 0.0346 511.7 1.8657 0.8510 1.1059 155.1 185190 0.0365 516.2 1.8774 0.8540 1.1031 156.7 0.0351 515.9 1.8749 0.8547 1.1046 156.4 190195 0.0370 520.5 1.8866 0.8578 1.1019 157.9 0.0355 520.2 1.8841 0.8585 1.1033 157.6 195200 0.0375 524.8 1.8958 0.8616 1.1007 159.2 0.0360 524.5 1.8933 0.8623 1.1021 158.9 200205 0.0380 529.1 1.9048 0.8654 1.0996 160.4 0.0365 528.8 1.9024 0.8661 1.1010 160.1 205210 0.0385 533.4 1.9139 0.8693 1.0985 161.6 0.0370 533.2 1.9114 0.8700 1.0998 161.4 210215 0.0390 537.8 1.9228 0.8731 1.0975 162.8 0.0375 537.5 1.9204 0.8738 1.0987 162.6 215220 0.0395 542.2 1.9318 0.8769 1.0964 164.0 0.0380 541.9 1.9293 0.8776 1.0976 163.7 220225 0.0400 546.5 1.9406 0.8807 1.0954 165.1 0.0385 546.3 1.9382 0.8814 1.0966 164.9 225230 0.0405 551.0 1.9494 0.8845 1.0944 166.3 0.0389 550.7 1.9470 0.8851 1.0956 166.1 230235 0.0410 555.4 1.9582 0.8882 1.0934 167.4 0.0394 555.2 1.9558 0.8889 1.0945 167.2 235240 0.0415 559.8 1.9669 0.8919 1.0925 168.5 0.0399 559.6 1.9645 0.8925 1.0935 168.3 240245 0.0420 564.3 1.9756 0.8955 1.0915 169.6 0.0404 564.1 1.9732 0.8962 1.0926 169.5 245

21

Page 24: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 750.00 kPa (abs) PRESSURE = 800.00 kPa (abs)

PRESSURE = 725.00 kPa (abs)PRESSURE = 700.00 kPa (abs)

94.83 0.0008 298.9 1.3075 1.1396 1.4679 443.6 SAT LIQ 0.0008 300.7 1.3122 1.1418 1.4700 437.8 96.3794.83 0.0240 436.1 1.6804 0.8539 1.1687 126.1 SAT VAP 0.0231 437.0 1.6810 0.8579 1.1720 125.8 96.37

95 0.0240 436.3 1.6808 0.8535 1.1684 126.2 — — — — — — 95100 0.0246 440.5 1.6922 0.8441 1.1597 128.2 0.0235 440.1 1.6894 0.8505 1.1652 127.4 100105 0.0251 444.7 1.7034 0.8371 1.1524 130.2 0.0241 444.3 1.7006 0.8424 1.1572 129.4 105110 0.0257 448.9 1.7144 0.8321 1.1463 132.1 0.0246 448.5 1.7117 0.8365 1.1505 131.3 110115 0.0262 453.1 1.7251 0.8285 1.1412 133.9 0.0252 452.7 1.7225 0.8323 1.1449 133.2 115120 0.0268 457.2 1.7357 0.8263 1.1367 135.6 0.0257 456.8 1.7331 0.8296 1.1401 134.9 120125 0.0273 461.3 1.7462 0.8252 1.1329 137.3 0.0262 461.0 1.7436 0.8280 1.1360 136.6 125130 0.0278 465.5 1.7565 0.8249 1.1295 138.9 0.0267 465.1 1.7539 0.8273 1.1323 138.3 130135 0.0283 469.6 1.7666 0.8254 1.1265 140.5 0.0272 469.2 1.7641 0.8275 1.1291 139.9 135140 0.0288 473.7 1.7767 0.8265 1.1238 142.1 0.0277 473.4 1.7742 0.8283 1.1262 141.5 140145 0.0293 477.8 1.7866 0.8281 1.1214 143.6 0.0282 477.5 1.7842 0.8297 1.1237 143.1 145150 0.0298 482.0 1.7965 0.8301 1.1192 145.1 0.0287 481.7 1.7940 0.8316 1.1213 144.6 150155 0.0303 486.1 1.8063 0.8326 1.1171 146.5 0.0292 485.8 1.8038 0.8339 1.1192 146.1 155160 0.0308 490.3 1.8159 0.8353 1.1153 147.9 0.0296 490.0 1.8135 0.8365 1.1172 147.5 160165 0.0313 494.5 1.8255 0.8382 1.1135 149.4 0.0301 494.2 1.8231 0.8393 1.1154 148.9 165170 0.0318 498.7 1.8351 0.8414 1.1119 150.7 0.0306 498.4 1.8327 0.8424 1.1137 150.3 170175 0.0323 502.9 1.8445 0.8448 1.1103 152.1 0.0311 502.6 1.8421 0.8457 1.1120 151.7 175180 0.0328 507.1 1.8539 0.8482 1.1089 153.4 0.0315 506.9 1.8516 0.8491 1.1105 153.1 180185 0.0332 511.4 1.8633 0.8518 1.1075 154.8 0.0320 511.1 1.8609 0.8527 1.1090 154.4 185190 0.0337 515.7 1.8725 0.8555 1.1061 156.1 0.0325 515.4 1.8702 0.8563 1.1076 155.7 190195 0.0342 519.9 1.8817 0.8593 1.1048 157.3 0.0329 519.7 1.8794 0.8600 1.1063 157.0 195200 0.0347 524.3 1.8909 0.8630 1.1035 158.6 0.0334 524.0 1.8885 0.8638 1.1050 158.3 200205 0.0351 528.6 1.9000 0.8668 1.1023 159.9 0.0339 528.3 1.8976 0.8676 1.1037 159.6 205210 0.0356 532.9 1.9090 0.8706 1.1012 161.1 0.0343 532.7 1.9067 0.8714 1.1025 160.8 210215 0.0361 537.3 1.9180 0.8745 1.1000 162.3 0.0348 537.0 1.9157 0.8752 1.1013 162.1 215220 0.0366 541.7 1.9269 0.8783 1.0989 163.5 0.0352 541.4 1.9246 0.8790 1.1001 163.3 220225 0.0370 546.1 1.9358 0.8821 1.0978 164.7 0.0357 545.8 1.9335 0.8827 1.0990 164.5 225230 0.0375 550.5 1.9446 0.8858 1.0967 165.9 0.0361 550.3 1.9423 0.8865 1.0979 165.7 230235 0.0380 554.9 1.9534 0.8895 1.0957 167.0 0.0366 554.7 1.9511 0.8902 1.0968 166.8 235240 0.0384 559.4 1.9621 0.8932 1.0947 168.2 0.0370 559.2 1.9598 0.8939 1.0958 168.0 240245 0.0389 563.9 1.9708 0.8969 1.0936 169.3 0.0375 563.6 1.9685 0.8975 1.0947 169.1 245250 — — — — — — 0.0379 568.1 1.9772 0.9011 1.0937 170.3 250

97.86 0.0008 302.4 1.3167 1.1440 1.4720 432.1 SAT LIQ 0.0008 305.7 1.3255 1.1486 1.4762 421.2 100.7497.86 0.0223 437.8 1.6816 0.8620 1.1754 125.6 SAT VAP 0.0209 439.3 1.6828 0.8701 1.1822 125.0 100.74

100 0.0226 439.6 1.6866 0.8572 1.1710 126.5 — — — — — — 100105 0.0231 443.9 1.6979 0.8480 1.1622 128.6 0.0214 442.9 1.6926 0.8603 1.1732 126.9 105110 0.0237 448.1 1.7090 0.8412 1.1549 130.5 0.0219 447.2 1.7038 0.8515 1.1645 129.0 110115 0.0242 452.3 1.7199 0.8363 1.1488 132.4 0.0224 451.5 1.7148 0.8450 1.1572 131.0 115120 0.0247 456.4 1.7306 0.8330 1.1436 134.3 0.0229 455.7 1.7256 0.8403 1.1511 132.9 120125 0.0252 460.6 1.7411 0.8309 1.1391 136.0 0.0234 459.9 1.7362 0.8372 1.1459 134.7 125130 0.0257 464.8 1.7514 0.8299 1.1352 137.7 0.0238 464.1 1.7466 0.8353 1.1414 136.5 130135 0.0262 468.9 1.7617 0.8297 1.1318 139.4 0.0243 468.2 1.7569 0.8344 1.1374 138.2 135140 0.0267 473.1 1.7718 0.8303 1.1288 141.0 0.0248 472.4 1.7671 0.8344 1.1340 139.9 140145 0.0271 477.2 1.7818 0.8315 1.1260 142.6 0.0252 476.6 1.7771 0.8351 1.1309 141.5 145150 0.0276 481.4 1.7916 0.8331 1.1235 144.1 0.0257 480.7 1.7870 0.8364 1.1281 143.1 150155 0.0281 485.5 1.8014 0.8352 1.1213 145.6 0.0261 484.9 1.7969 0.8381 1.1256 144.7 155160 0.0285 489.7 1.8112 0.8377 1.1192 147.1 0.0266 489.1 1.8066 0.8403 1.1233 146.2 160165 0.0290 493.9 1.8208 0.8405 1.1173 148.5 0.0270 493.3 1.8163 0.8428 1.1212 147.7 165170 0.0295 498.1 1.8303 0.8435 1.1155 150.0 0.0275 497.6 1.8258 0.8456 1.1192 149.2 170175 0.0299 502.4 1.8398 0.8467 1.1138 151.4 0.0279 501.8 1.8354 0.8487 1.1173 150.6 175180 0.0304 506.6 1.8492 0.8500 1.1122 152.7 0.0283 506.0 1.8448 0.8519 1.1156 152.0 180185 0.0308 510.9 1.8586 0.8535 1.1106 154.1 0.0288 510.3 1.8542 0.8553 1.1139 153.4 185190 0.0313 515.1 1.8679 0.8571 1.1092 155.4 0.0292 514.6 1.8635 0.8588 1.1123 154.8 190195 0.0318 519.4 1.8771 0.8608 1.1078 156.7 0.0296 518.9 1.8727 0.8624 1.1108 156.1 195200 0.0322 523.7 1.8863 0.8645 1.1064 158.0 0.0301 523.2 1.8819 0.8661 1.1093 157.5 200205 0.0327 528.1 1.8954 0.8683 1.1051 159.3 0.0305 527.6 1.8910 0.8698 1.1079 158.8 205210 0.0331 532.4 1.9044 0.8721 1.1038 160.6 0.0309 531.9 1.9001 0.8735 1.1066 160.1 210215 0.0335 536.8 1.9134 0.8759 1.1026 161.8 0.0313 536.3 1.9091 0.8773 1.1053 161.3 215220 0.0340 541.2 1.9224 0.8797 1.1014 163.0 0.0317 540.7 1.9180 0.8811 1.1040 162.6 220225 0.0344 545.6 1.9313 0.8834 1.1002 164.3 0.0322 545.1 1.9269 0.8848 1.1027 163.8 225230 0.0349 550.0 1.9401 0.8872 1.0991 165.5 0.0326 549.5 1.9358 0.8886 1.1015 165.0 230235 0.0353 554.5 1.9489 0.8909 1.0980 166.6 0.0330 554.0 1.9446 0.8923 1.1003 166.2 235240 0.0358 558.9 1.9576 0.8946 1.0969 167.8 0.0334 558.5 1.9534 0.8960 1.0991 167.4 240245 0.0362 563.4 1.9663 0.8982 1.0958 169.0 0.0338 563.0 1.9621 0.8996 1.0980 168.6 245250 0.0366 567.9 1.9750 0.9018 1.0948 170.1 0.0342 567.5 1.9707 0.9032 1.0969 169.8 250255 — — — — — — 0.0347 572.0 1.9793 0.9068 1.0958 170.9 255

22

Page 25: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 900.00 kPa (abs)PRESSURE = 850.00 kPa (abs)

PRESSURE = 950.00 kPa (abs) PRESSURE = 1000.00 kPa (abs)

103.49 0.0008 308.8 1.3338 1.1532 1.4806 410.8 SAT LIQ 0.0008 311.9 1.3417 1.1579 1.4852 400.8 106.12103.49 0.0196 440.7 1.6838 0.8782 1.1894 124.4 SAT VAP 0.0185 442.0 1.6848 0.8865 1.1968 123.8 106.12

105 0.0198 442.0 1.6873 0.8742 1.1857 125.1 — — — — — — 105110 0.0203 446.3 1.6987 0.8629 1.1751 127.4 0.0189 445.4 1.6938 0.8759 1.1871 125.7 110115 0.0208 450.6 1.7099 0.8545 1.1665 129.5 0.0194 449.8 1.7051 0.8652 1.1767 127.9 115120 0.0213 454.9 1.7208 0.8484 1.1592 131.5 0.0198 454.1 1.7161 0.8574 1.1682 130.0 120125 0.0217 459.1 1.7315 0.8441 1.1532 133.4 0.0203 458.3 1.7269 0.8516 1.1610 132.0 125130 0.0222 463.3 1.7420 0.8412 1.1480 135.3 0.0207 462.6 1.7375 0.8476 1.1550 134.0 130135 0.0226 467.5 1.7523 0.8395 1.1434 137.0 0.0212 466.8 1.7479 0.8451 1.1498 135.8 135140 0.0231 471.7 1.7625 0.8388 1.1395 138.8 0.0216 471.0 1.7582 0.8436 1.1454 137.7 140145 0.0235 475.9 1.7726 0.8390 1.1360 140.5 0.0220 475.3 1.7683 0.8432 1.1414 139.4 145150 0.0240 480.1 1.7826 0.8398 1.1329 142.1 0.0224 479.5 1.7784 0.8435 1.1379 141.1 150155 0.0244 484.3 1.7925 0.8412 1.1301 143.7 0.0229 483.7 1.7883 0.8445 1.1348 142.8 155160 0.0248 488.5 1.8023 0.8431 1.1275 145.3 0.0233 487.9 1.7981 0.8460 1.1319 144.4 160165 0.0252 492.8 1.8119 0.8453 1.1252 146.8 0.0237 492.2 1.8078 0.8480 1.1293 146.0 165170 0.0257 497.0 1.8216 0.8479 1.1230 148.3 0.0241 496.4 1.8174 0.8503 1.1269 147.5 170175 0.0261 501.2 1.8311 0.8508 1.1210 149.8 0.0245 500.7 1.8270 0.8530 1.1247 149.0 175180 0.0265 505.5 1.8405 0.8539 1.1190 151.3 0.0249 504.9 1.8365 0.8559 1.1226 150.5 180185 0.0269 509.8 1.8499 0.8571 1.1173 152.7 0.0253 509.2 1.8459 0.8590 1.1207 152.0 185190 0.0273 514.1 1.8593 0.8605 1.1155 154.1 0.0257 513.5 1.8552 0.8623 1.1188 153.4 190195 0.0277 518.4 1.8685 0.8640 1.1139 155.5 0.0261 517.8 1.8645 0.8657 1.1171 154.9 195200 0.0281 522.7 1.8777 0.8676 1.1123 156.9 0.0265 522.2 1.8737 0.8693 1.1154 156.3 200205 0.0286 527.1 1.8868 0.8713 1.1108 158.2 0.0268 526.5 1.8829 0.8729 1.1138 157.6 205210 0.0290 531.4 1.8959 0.8750 1.1094 159.5 0.0272 530.9 1.8920 0.8766 1.1122 159.0 210215 0.0294 535.8 1.9050 0.8788 1.1079 160.8 0.0276 535.3 1.9010 0.8803 1.1107 160.3 215220 0.0298 540.2 1.9139 0.8825 1.1066 162.1 0.0280 539.7 1.9100 0.8840 1.1092 161.6 220225 0.0302 544.6 1.9229 0.8863 1.1052 163.4 0.0284 544.1 1.9190 0.8877 1.1078 162.9 225230 0.0306 549.1 1.9317 0.8900 1.1039 164.6 0.0288 548.6 1.9278 0.8914 1.1064 164.2 230235 0.0310 553.5 1.9405 0.8937 1.1027 165.8 0.0291 553.1 1.9367 0.8951 1.1050 165.4 235240 0.0314 558.0 1.9493 0.8974 1.1014 167.1 0.0295 557.5 1.9455 0.8988 1.1037 166.7 240245 0.0317 562.5 1.9580 0.9010 1.1002 168.2 0.0299 562.0 1.9542 0.9025 1.1024 167.9 245250 0.0321 567.0 1.9667 0.9046 1.0990 169.4 0.0303 566.6 1.9629 0.9061 1.1012 169.1 250255 0.0325 571.5 1.9753 0.9082 1.0978 170.6 0.0306 571.1 1.9715 0.9096 1.0999 170.3 255260 — — — — — — 0.0310 575.7 1.9801 0.9131 1.0987 171.4 260

108.64 0.0008 314.8 1.3493 1.1627 1.4900 391.3 SAT LIQ 0.0008 317.6 1.3565 1.1678 1.4951 382.2 111.07108.64 0.0175 443.2 1.6857 0.8948 1.2045 123.2 SAT VAP 0.0166 444.4 1.6866 0.9034 1.2125 122.6 111.07

110 0.0176 444.5 1.6889 0.8905 1.2006 123.9 — — — — — — 110115 0.0181 448.9 1.7004 0.8772 1.1881 126.3 0.0169 448.0 1.6957 0.8908 1.2009 124.6 115120 0.0185 453.2 1.7115 0.8673 1.1780 128.5 0.0174 452.4 1.7070 0.8784 1.1889 127.0 120125 0.0190 457.6 1.7224 0.8600 1.1696 130.6 0.0178 456.7 1.7181 0.8692 1.1790 129.2 125130 0.0194 461.8 1.7331 0.8547 1.1626 132.7 0.0182 461.1 1.7289 0.8625 1.1709 131.3 130135 0.0198 466.1 1.7436 0.8511 1.1567 134.6 0.0186 465.4 1.7395 0.8577 1.1640 133.4 135140 0.0203 470.4 1.7540 0.8488 1.1516 136.5 0.0191 469.7 1.7499 0.8545 1.1582 135.3 140145 0.0207 474.6 1.7642 0.8477 1.1471 138.3 0.0195 473.9 1.7602 0.8526 1.1531 137.2 145150 0.0211 478.8 1.7743 0.8475 1.1432 140.1 0.0198 478.2 1.7703 0.8517 1.1487 139.0 150155 0.0215 483.1 1.7842 0.8480 1.1397 141.8 0.0202 482.4 1.7803 0.8517 1.1448 140.8 155160 0.0219 487.3 1.7941 0.8491 1.1365 143.5 0.0206 486.7 1.7902 0.8524 1.1413 142.5 160165 0.0223 491.6 1.8038 0.8508 1.1336 145.1 0.0210 491.0 1.8000 0.8537 1.1381 144.2 165170 0.0227 495.8 1.8135 0.8529 1.1310 146.7 0.0214 495.2 1.8097 0.8555 1.1353 145.8 170175 0.0230 500.1 1.8231 0.8553 1.1286 148.3 0.0217 499.5 1.8193 0.8577 1.1326 147.5 175180 0.0234 504.4 1.8326 0.8580 1.1263 149.8 0.0221 503.8 1.8288 0.8603 1.1301 149.0 180185 0.0238 508.7 1.8420 0.8610 1.1242 151.3 0.0225 508.1 1.8383 0.8631 1.1278 150.6 185190 0.0242 513.0 1.8514 0.8642 1.1222 152.8 0.0229 512.4 1.8477 0.8661 1.1257 152.1 190195 0.0246 517.3 1.8607 0.8675 1.1203 154.2 0.0232 516.8 1.8570 0.8693 1.1236 153.6 195200 0.0249 521.7 1.8699 0.8710 1.1185 155.6 0.0236 521.1 1.8662 0.8727 1.1217 155.0 200205 0.0253 526.0 1.8791 0.8745 1.1167 157.0 0.0239 525.5 1.8754 0.8762 1.1198 156.5 205210 0.0257 530.4 1.8882 0.8781 1.1151 158.4 0.0243 529.9 1.8846 0.8797 1.1180 157.9 210215 0.0261 534.8 1.8973 0.8818 1.1135 159.8 0.0246 534.3 1.8936 0.8834 1.1163 159.3 215220 0.0264 539.2 1.9063 0.8855 1.1119 161.1 0.0250 538.7 1.9027 0.8870 1.1146 160.6 220225 0.0268 543.7 1.9152 0.8892 1.1104 162.4 0.0254 543.2 1.9116 0.8907 1.1130 162.0 225230 0.0272 548.1 1.9241 0.8929 1.1089 163.7 0.0257 547.6 1.9205 0.8944 1.1114 163.3 230235 0.0275 552.6 1.9330 0.8966 1.1075 165.0 0.0261 552.1 1.9294 0.8981 1.1099 164.6 235240 0.0279 557.1 1.9418 0.9003 1.1061 166.3 0.0264 556.6 1.9382 0.9017 1.1084 165.9 240245 0.0282 561.6 1.9505 0.9039 1.1047 167.5 0.0268 561.1 1.9470 0.9054 1.1070 167.1 245250 0.0286 566.1 1.9592 0.9075 1.1034 168.7 0.0271 565.7 1.9557 0.9090 1.1056 168.4 250255 0.0290 570.7 1.9679 0.9111 1.1021 169.9 0.0274 570.2 1.9644 0.9125 1.1042 169.6 255260 0.0293 575.2 1.9765 0.9146 1.1008 171.1 0.0278 574.8 1.9730 0.9161 1.1029 170.8 260265 — — — — — — 0.0281 579.4 1.9815 0.9195 1.1015 172.0 265

23

Page 26: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 1200.00 kPa (abs)

PRESSURE = 1300.00 kPa (abs)

PRESSURE = 1100.00 kPa (abs)

115.67 0.0008 323.0 1.3702 1.1785 1.5059 364.8 SAT LIQ 0.0009 328.0 1.3829 1.1903 1.5178 348.7 119.96115.67 0.0149 446.6 1.6881 0.9210 1.2295 121.4 SAT LIQ 0.0136 448.5 1.6895 0.9395 1.2480 120.1 119.96

120 0.0153 450.6 1.6983 0.9050 1.2146 123.7 0.0136 448.6 1.6896 0.9393 1.2478 120.1 120125 0.0158 455.0 1.7096 0.8909 1.2008 126.2 0.0140 453.2 1.7013 0.9183 1.2279 122.9 125130 0.0162 459.5 1.7206 0.8805 1.1897 128.5 0.0144 457.8 1.7126 0.9027 1.2124 125.5 130135 0.0166 463.8 1.7315 0.8728 1.1805 130.8 0.0148 462.3 1.7237 0.8911 1.2000 128.0 135140 0.0170 468.2 1.7420 0.8673 1.1729 132.9 0.0152 466.7 1.7345 0.8827 1.1899 130.3 140145 0.0173 472.5 1.7525 0.8636 1.1664 134.9 0.0156 471.1 1.7451 0.8765 1.1814 132.5 145150 0.0177 476.8 1.7627 0.8612 1.1607 136.9 0.0159 475.5 1.7555 0.8723 1.1743 134.6 150155 0.0181 481.1 1.7728 0.8600 1.1558 138.8 0.0163 479.8 1.7657 0.8696 1.1681 136.6 155160 0.0184 485.4 1.7828 0.8597 1.1515 140.6 0.0166 484.2 1.7758 0.8681 1.1628 138.6 160165 0.0188 489.7 1.7927 0.8602 1.1477 142.4 0.0170 488.5 1.7857 0.8676 1.1580 140.5 165170 0.0192 494.0 1.8024 0.8613 1.1442 144.1 0.0173 492.8 1.7956 0.8679 1.1538 142.3 170175 0.0195 498.4 1.8121 0.8630 1.1410 145.8 0.0176 497.2 1.8053 0.8689 1.1500 144.1 175180 0.0199 502.7 1.8217 0.8651 1.1381 147.5 0.0180 501.5 1.8150 0.8704 1.1466 145.9 180185 0.0202 507.0 1.8312 0.8675 1.1354 149.1 0.0183 505.9 1.8245 0.8724 1.1434 147.6 185190 0.0205 511.3 1.8406 0.8703 1.1329 150.7 0.0186 510.2 1.8340 0.8747 1.1404 149.2 190195 0.0209 515.7 1.8500 0.8732 1.1305 152.2 0.0189 514.6 1.8434 0.8774 1.1377 150.9 195200 0.0212 520.1 1.8593 0.8764 1.1282 153.8 0.0192 519.0 1.8528 0.8803 1.1351 152.4 200205 0.0216 524.5 1.8685 0.8797 1.1261 155.2 0.0196 523.4 1.8620 0.8834 1.1327 154.0 205210 0.0219 528.9 1.8777 0.8831 1.1241 156.7 0.0199 527.9 1.8712 0.8866 1.1304 155.5 210215 0.0222 533.3 1.8868 0.8866 1.1221 158.2 0.0202 532.3 1.8804 0.8900 1.1281 157.0 215220 0.0225 537.7 1.8958 0.8902 1.1202 159.6 0.0205 536.8 1.8895 0.8935 1.1260 158.5 220225 0.0229 542.2 1.9048 0.8938 1.1184 161.0 0.0208 541.2 1.8985 0.8970 1.1240 160.0 225230 0.0232 546.7 1.9138 0.8974 1.1167 162.4 0.0211 545.7 1.9075 0.9006 1.1220 161.4 230235 0.0235 551.2 1.9227 0.9011 1.1149 163.7 0.0214 550.2 1.9164 0.9042 1.1201 162.8 235240 0.0239 555.7 1.9315 0.9047 1.1133 165.0 0.0217 554.8 1.9253 0.9078 1.1183 164.2 240245 0.0242 560.2 1.9403 0.9083 1.1117 166.4 0.0220 559.3 1.9341 0.9114 1.1165 165.5 245250 0.0245 564.8 1.9490 0.9119 1.1101 167.6 0.0223 563.9 1.9429 0.9149 1.1147 166.9 250255 0.0248 569.3 1.9577 0.9155 1.1086 168.9 0.0226 568.5 1.9516 0.9185 1.1130 168.2 255260 0.0251 573.9 1.9664 0.9190 1.1071 170.2 0.0229 573.1 1.9602 0.9220 1.1114 169.5 260265 0.0254 578.5 1.9750 0.9225 1.1056 171.4 0.0232 577.7 1.9689 0.9255 1.1098 170.8 265270 0.0258 583.2 1.9835 0.9259 1.1042 172.6 0.0235 582.3 1.9775 0.9289 1.1082 172.0 270

124 0.0009 332.8 1.3948 1.2032 1.5309 333.5 SAT LIQ 0.0009 337.4 1.4060 1.2175 1.5455 319.1 127.81124 0.0125 450.3 1.6906 0.9593 1.2681 118.8 SAT VAP 0.0115 451.9 1.6915 0.9804 1.2900 117.4 127.81125 0.0125 451.2 1.6930 0.9537 1.2628 119.4 — — — — — — 125130 0.0129 456.0 1.7047 0.9306 1.2407 122.3 0.0116 454.0 1.6968 0.9667 1.2769 118.9 130135 0.0133 460.6 1.7161 0.9137 1.2235 125.1 0.0120 458.8 1.7086 0.9419 1.2526 121.9 135140 0.0137 465.1 1.7272 0.9011 1.2099 127.6 0.0124 463.4 1.7199 0.9238 1.2339 124.7 140145 0.0141 469.6 1.7379 0.8919 1.1988 130.0 0.0127 468.0 1.7310 0.9104 1.2192 127.3 145150 0.0144 474.0 1.7485 0.8853 1.1896 132.3 0.0131 472.5 1.7417 0.9006 1.2072 129.8 150155 0.0147 478.4 1.7589 0.8807 1.1818 134.4 0.0134 477.0 1.7523 0.8936 1.1973 132.1 155160 0.0151 482.8 1.7691 0.8776 1.1751 136.5 0.0137 481.5 1.7626 0.8887 1.1890 134.4 160165 0.0154 487.2 1.7791 0.8759 1.1694 138.5 0.0141 485.9 1.7728 0.8854 1.1818 136.5 165170 0.0157 491.6 1.7891 0.8752 1.1642 140.5 0.0144 490.3 1.7828 0.8835 1.1756 138.6 170175 0.0160 496.0 1.7989 0.8754 1.1597 142.4 0.0147 494.7 1.7927 0.8827 1.1702 140.6 175180 0.0164 500.3 1.8086 0.8762 1.1556 144.2 0.0150 499.1 1.8025 0.8827 1.1653 142.5 180185 0.0167 504.7 1.8182 0.8777 1.1519 146.0 0.0153 503.6 1.8122 0.8835 1.1609 144.4 185190 0.0170 509.1 1.8278 0.8796 1.1484 147.7 0.0156 508.0 1.8218 0.8849 1.1569 146.2 190195 0.0173 513.5 1.8372 0.8819 1.1453 149.4 0.0158 512.4 1.8313 0.8867 1.1533 148.0 195200 0.0176 517.9 1.8466 0.8845 1.1423 151.1 0.0161 516.9 1.8408 0.8890 1.1499 149.7 200205 0.0179 522.4 1.8559 0.8873 1.1395 152.7 0.0164 521.3 1.8501 0.8915 1.1467 151.4 205210 0.0182 526.8 1.8652 0.8904 1.1369 154.3 0.0167 525.8 1.8594 0.8943 1.1437 153.1 210215 0.0185 531.3 1.8743 0.8936 1.1344 155.9 0.0170 530.2 1.8686 0.8974 1.1409 154.7 215220 0.0188 535.8 1.8835 0.8969 1.1320 157.4 0.0173 534.7 1.8778 0.9005 1.1382 156.3 220225 0.0190 540.2 1.8925 0.9003 1.1297 158.9 0.0175 539.3 1.8869 0.9038 1.1357 157.9 225230 0.0193 544.8 1.9015 0.9038 1.1275 160.4 0.0178 543.8 1.8959 0.9072 1.1332 159.4 230235 0.0196 549.3 1.9105 0.9074 1.1254 161.9 0.0181 548.3 1.9049 0.9106 1.1309 160.9 235240 0.0199 553.8 1.9194 0.9109 1.1234 163.3 0.0184 552.9 1.9138 0.9141 1.1286 162.4 240245 0.0202 558.4 1.9283 0.9145 1.1214 164.7 0.0186 557.5 1.9227 0.9176 1.1264 163.9 245250 0.0205 563.0 1.9370 0.9180 1.1195 166.1 0.0189 562.1 1.9316 0.9212 1.1243 165.3 250255 0.0208 567.6 1.9458 0.9215 1.1176 167.5 0.0192 566.7 1.9403 0.9247 1.1223 166.7 255260 0.0210 572.2 1.9545 0.9251 1.1158 168.8 0.0194 571.3 1.9491 0.9282 1.1203 168.1 260265 0.0213 576.8 1.9631 0.9285 1.1140 170.1 0.0197 576.0 1.9577 0.9316 1.1183 169.4 265270 0.0216 581.5 1.9717 0.9319 1.1123 171.4 0.0200 580.6 1.9664 0.9350 1.1164 170.8 270275 0.0219 586.1 1.9803 0.9353 1.1106 172.7 0.0202 585.3 1.9750 0.9384 1.1146 172.1 275280 — — — — — — 0.0205 590.0 1.9835 0.9417 1.1128 173.4 280

PRESSURE = 1400.00 kPa (abs)

24

Page 27: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 1600.00 kPa (abs)PRESSURE = 1500.00 kPa (abs)

PRESSURE = 1700.00 kPa (abs) PRESSURE = 1800.00 kPa (abs)

131.42 0.0009 341.8 1.4167 1.2333 1.5615 305.4 SAT LIQ 0.0009 346.0 1.4268 1.2508 1.5793 292.3 134.86131.42 0.0106 453.3 1.6923 1.0033 1.3140 116.0 SAT VAP 0.0098 454.5 1.6929 1.0283 1.3405 114.6 134.86

135 0.0109 456.8 1.7010 0.9783 1.2897 118.5 0.0098 454.7 1.6932 1.0270 1.3392 114.7 135140 0.0112 461.6 1.7127 0.9520 1.2635 121.6 0.0102 459.7 1.7055 0.9883 1.3011 118.3 140145 0.0116 466.3 1.7241 0.9330 1.2436 124.5 0.0106 464.6 1.7172 0.9610 1.2734 121.5 145150 0.0119 471.0 1.7351 0.9190 1.2278 127.2 0.0109 469.3 1.7285 0.9413 1.2523 124.5 150155 0.0123 475.5 1.7458 0.9088 1.2151 129.7 0.0112 474.0 1.7395 0.9269 1.2357 127.2 155160 0.0126 480.1 1.7563 0.9014 1.2046 132.1 0.0115 478.6 1.7502 0.9164 1.2223 129.8 160165 0.0129 484.6 1.7666 0.8963 1.1957 134.4 0.0119 483.2 1.7606 0.9089 1.2113 132.2 165170 0.0132 489.0 1.7768 0.8929 1.1881 136.6 0.0121 487.7 1.7709 0.9036 1.2020 134.5 170175 0.0135 493.5 1.7868 0.8909 1.1816 138.7 0.0124 492.2 1.7810 0.9001 1.1940 136.8 175180 0.0138 497.9 1.7967 0.8900 1.1758 140.7 0.0127 496.7 1.7910 0.8980 1.1871 138.9 180185 0.0141 502.4 1.8064 0.8900 1.1706 142.7 0.0130 501.2 1.8009 0.8971 1.1810 141.0 185190 0.0143 506.8 1.8161 0.8907 1.1660 144.6 0.0133 505.7 1.8106 0.8970 1.1756 143.0 190195 0.0146 511.3 1.8257 0.8920 1.1617 146.5 0.0135 510.2 1.8202 0.8977 1.1707 145.0 195200 0.0149 515.8 1.8351 0.8938 1.1578 148.3 0.0138 514.6 1.8298 0.8991 1.1662 146.9 200205 0.0152 520.2 1.8446 0.8960 1.1542 150.1 0.0141 519.1 1.8392 0.9008 1.1621 148.7 205210 0.0154 524.7 1.8539 0.8986 1.1509 151.8 0.0143 523.7 1.8486 0.9030 1.1583 150.5 210215 0.0157 529.2 1.8632 0.9013 1.1477 153.5 0.0146 528.2 1.8579 0.9055 1.1547 152.3 215220 0.0160 533.7 1.8724 0.9043 1.1447 155.2 0.0148 532.7 1.8672 0.9083 1.1514 154.0 220225 0.0162 538.3 1.8815 0.9074 1.1418 156.8 0.0151 537.3 1.8763 0.9112 1.1482 155.7 225230 0.0165 542.8 1.8906 0.9107 1.1391 158.4 0.0153 541.8 1.8855 0.9144 1.1452 157.3 230235 0.0168 547.4 1.8996 0.9141 1.1365 159.9 0.0156 546.4 1.8945 0.9176 1.1424 158.9 235240 0.0170 551.9 1.9086 0.9175 1.1340 161.5 0.0158 551.0 1.9035 0.9209 1.1396 160.5 240245 0.0173 556.5 1.9175 0.9209 1.1316 163.0 0.0161 555.6 1.9125 0.9243 1.1369 162.1 245250 0.0175 561.2 1.9263 0.9244 1.1293 164.4 0.0163 560.2 1.9213 0.9277 1.1344 163.6 250255 0.0178 565.8 1.9351 0.9278 1.1270 165.9 0.0166 564.9 1.9302 0.9311 1.1319 165.1 255260 0.0180 570.4 1.9439 0.9313 1.1249 167.3 0.0168 569.6 1.9390 0.9345 1.1296 166.5 260265 0.0183 575.1 1.9526 0.9347 1.1227 168.7 0.0170 574.2 1.9477 0.9379 1.1273 168.0 265270 0.0185 579.8 1.9613 0.9381 1.1207 170.1 0.0173 578.9 1.9564 0.9413 1.1250 169.4 270275 0.0188 584.5 1.9699 0.9415 1.1187 171.4 0.0175 583.6 1.9651 0.9446 1.1228 170.8 275280 0.0190 589.2 1.9784 0.9448 1.1167 172.8 0.0178 588.4 1.9736 0.9479 1.1207 172.1 280285 0.0193 593.9 1.9870 0.9481 1.1148 174.1 0.0180 593.1 1.9822 0.9512 1.1187 173.5 285

138.14 0.0009 350.0 1.4364 1.2703 1.5990 279.7 SAT LIQ 0.0009 353.9 1.4457 1.2920 1.6209 267.4 141.28138.14 0.0092 455.7 1.6933 1.0556 1.3698 113.2 SAT VAP 0.0085 456.7 1.6936 1.0859 1.4024 111.7 141.28

140 0.0093 457.6 1.6980 1.0365 1.3508 114.6 — — — — — — 140145 0.0097 462.7 1.7102 0.9967 1.3109 118.3 0.0088 460.6 1.7031 1.0438 1.3601 114.7 145150 0.0100 467.6 1.7219 0.9688 1.2820 121.5 0.0092 465.7 1.7152 1.0036 1.3191 118.4 150155 0.0103 472.4 1.7332 0.9487 1.2601 124.5 0.0095 470.7 1.7269 0.9755 1.2894 121.7 155160 0.0106 477.1 1.7441 0.9341 1.2428 127.3 0.0098 475.5 1.7381 0.9553 1.2668 124.7 160165 0.0109 481.7 1.7548 0.9235 1.2289 129.9 0.0101 480.2 1.7489 0.9407 1.2491 127.6 165170 0.0112 486.3 1.7652 0.9159 1.2174 132.4 0.0104 484.9 1.7595 0.9301 1.2349 130.2 170175 0.0115 490.9 1.7754 0.9106 1.2078 134.8 0.0107 489.5 1.7699 0.9225 1.2230 132.7 175180 0.0118 495.4 1.7855 0.9071 1.1995 137.1 0.0109 494.1 1.7801 0.9173 1.2130 135.1 180185 0.0120 500.0 1.7955 0.9050 1.1923 139.2 0.0112 498.7 1.7902 0.9138 1.2045 137.4 185190 0.0123 504.5 1.8053 0.9040 1.1859 141.3 0.0115 503.3 1.8001 0.9118 1.1970 139.6 190195 0.0126 509.0 1.8150 0.9040 1.1802 143.4 0.0117 507.8 1.8099 0.9108 1.1904 141.8 195200 0.0128 513.5 1.8246 0.9047 1.1751 145.4 0.0120 512.4 1.8196 0.9108 1.1845 143.8 200205 0.0131 518.0 1.8341 0.9060 1.1704 147.3 0.0122 516.9 1.8291 0.9116 1.1792 145.8 205210 0.0133 522.6 1.8435 0.9078 1.1661 149.2 0.0124 521.5 1.8386 0.9129 1.1743 147.8 210215 0.0136 527.1 1.8529 0.9100 1.1621 151.0 0.0127 526.1 1.8480 0.9147 1.1698 149.7 215220 0.0138 531.7 1.8622 0.9125 1.1584 152.8 0.0129 530.6 1.8574 0.9169 1.1656 151.5 220225 0.0141 536.2 1.8714 0.9152 1.1549 154.5 0.0132 535.2 1.8666 0.9194 1.1617 153.3 225230 0.0143 540.8 1.8806 0.9181 1.1515 156.2 0.0134 539.8 1.8758 0.9221 1.1580 155.1 230235 0.0145 545.4 1.8896 0.9212 1.1483 157.9 0.0136 544.5 1.8849 0.9250 1.1546 156.8 235240 0.0148 550.0 1.8987 0.9244 1.1453 159.5 0.0139 549.1 1.8940 0.9281 1.1512 158.5 240245 0.0150 554.7 1.9077 0.9277 1.1424 161.1 0.0141 553.7 1.9030 0.9313 1.1481 160.2 245250 0.0153 559.3 1.9166 0.9310 1.1396 162.7 0.0143 558.4 1.9120 0.9345 1.1450 161.8 250255 0.0155 564.0 1.9255 0.9344 1.1370 164.2 0.0145 563.1 1.9209 0.9378 1.1421 163.4 255260 0.0157 568.7 1.9343 0.9378 1.1344 165.7 0.0148 567.8 1.9297 0.9411 1.1393 164.9 260265 0.0160 573.4 1.9431 0.9411 1.1319 167.2 0.0150 572.5 1.9386 0.9444 1.1366 166.4 265270 0.0162 578.1 1.9518 0.9445 1.1294 168.7 0.0152 577.2 1.9473 0.9477 1.1340 167.9 270275 0.0164 582.8 1.9604 0.9478 1.1271 170.1 0.0154 582.0 1.9560 0.9510 1.1314 169.4 275280 0.0166 587.6 1.9691 0.9511 1.1248 171.5 0.0156 586.7 1.9646 0.9543 1.1290 170.8 280285 0.0169 592.3 1.9776 0.9543 1.1226 172.9 0.0158 591.5 1.9733 0.9575 1.1266 172.2 285290 0.0171 597.1 1.9862 0.9575 1.1204 174.2 0.0161 596.3 1.9818 0.9607 1.1243 173.6 290295 — — — — — — 0.0163 601.1 1.9903 0.9638 1.1220 175.0 295

25

Page 28: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 2000.00 kPa (abs)PRESSURE = 1900.00 kPa (abs)

PRESSURE = 2200.00 kPa (abs) PRESSURE = 2400.00 kPa (abs)

144.29 0.0009 357.7 1.4547 1.3162 1.6453 255.6 SAT LIQ 0.0010 361.5 1.4633 1.3435 1.6727 243.9 147.19144.29 0.0080 457.5 1.6937 1.1198 1.4391 110.2 SAT VAP 0.0075 458.3 1.6937 1.1579 1.4806 108.6 147.19

145 0.0080 458.3 1.6956 1.1089 1.4281 110.8 — — — — — — 145150 0.0084 463.7 1.7084 1.0490 1.3671 115.0 0.0077 461.5 1.7012 1.1107 1.4324 111.3 150155 0.0087 468.8 1.7205 1.0090 1.3257 118.7 0.0081 466.9 1.7139 1.0522 1.3720 115.4 155160 0.0091 473.8 1.7320 0.9811 1.2956 122.0 0.0084 472.0 1.7259 1.0131 1.3306 119.1 160165 0.0094 478.7 1.7432 0.9612 1.2727 125.1 0.0087 477.0 1.7373 0.9858 1.3005 122.4 165170 0.0096 483.4 1.7540 0.9467 1.2547 127.9 0.0090 481.9 1.7484 0.9663 1.2775 125.5 170175 0.0099 488.1 1.7645 0.9362 1.2400 130.6 0.0092 486.7 1.7592 0.9522 1.2594 128.4 175180 0.0102 492.8 1.7749 0.9288 1.2280 133.1 0.0095 491.4 1.7697 0.9420 1.2447 131.1 180185 0.0104 497.4 1.7850 0.9237 1.2178 135.6 0.0097 496.1 1.7800 0.9348 1.2324 133.6 185190 0.0107 502.0 1.7950 0.9203 1.2090 137.9 0.0100 500.8 1.7901 0.9299 1.2220 136.1 190195 0.0109 506.6 1.8049 0.9184 1.2013 140.1 0.0102 505.4 1.8001 0.9267 1.2131 138.4 195200 0.0112 511.2 1.8147 0.9175 1.1946 142.3 0.0105 510.0 1.8099 0.9248 1.2052 140.7 200205 0.0114 515.8 1.8243 0.9176 1.1885 144.4 0.0107 514.7 1.8196 0.9241 1.1983 142.8 205210 0.0117 520.4 1.8339 0.9184 1.1829 146.4 0.0109 519.3 1.8292 0.9242 1.1920 144.9 210215 0.0119 525.0 1.8433 0.9197 1.1779 148.3 0.0112 523.9 1.8387 0.9251 1.1863 147.0 215220 0.0121 529.6 1.8527 0.9216 1.1732 150.3 0.0114 528.5 1.8482 0.9265 1.1811 149.0 220225 0.0123 534.2 1.8620 0.9238 1.1689 152.1 0.0116 533.2 1.8575 0.9284 1.1763 150.9 225230 0.0126 538.8 1.8712 0.9262 1.1648 153.9 0.0118 537.8 1.8668 0.9306 1.1718 152.8 230235 0.0128 543.5 1.8804 0.9290 1.1610 155.7 0.0121 542.5 1.8760 0.9331 1.1676 154.6 235240 0.0130 548.1 1.8895 0.9319 1.1573 157.5 0.0123 547.2 1.8852 0.9358 1.1636 156.4 240245 0.0132 552.8 1.8986 0.9349 1.1539 159.2 0.0125 551.8 1.8943 0.9387 1.1598 158.2 245250 0.0135 557.5 1.9076 0.9380 1.1506 160.8 0.0127 556.5 1.9033 0.9417 1.1562 159.9 250255 0.0137 562.2 1.9165 0.9412 1.1474 162.5 0.0129 561.3 1.9123 0.9448 1.1528 161.5 255260 0.0139 566.9 1.9254 0.9445 1.1443 164.1 0.0131 566.0 1.9212 0.9480 1.1495 163.2 260265 0.0141 571.6 1.9342 0.9478 1.1414 165.6 0.0133 570.7 1.9300 0.9512 1.1463 164.8 265270 0.0143 576.4 1.9430 0.9510 1.1386 167.2 0.0135 575.5 1.9389 0.9544 1.1433 166.4 270275 0.0145 581.1 1.9517 0.9543 1.1359 168.7 0.0137 580.3 1.9476 0.9576 1.1404 167.9 275280 0.0147 585.9 1.9604 0.9575 1.1332 170.1 0.0139 585.1 1.9563 0.9608 1.1375 169.4 280285 0.0149 590.7 1.9690 0.9608 1.1306 171.6 0.0141 589.9 1.9650 0.9640 1.1348 170.9 285290 0.0151 595.5 1.9776 0.9639 1.1281 173.0 0.0143 594.7 1.9736 0.9672 1.1321 172.4 290295 0.0154 600.3 1.9862 0.9670 1.1257 174.4 0.0145 599.6 1.9822 0.9702 1.1295 173.8 295300 — — — — — — 0.0147 604.4 1.9907 0.9733 1.1270 175.2 300

152.66 0.0010 368.6 1.4798 1.4090 1.7385 221.3 SAT LIQ 0.0010 375.6 1.4955 1.4949 1.8245 199.2 157.76152.66 0.0066 459.5 1.6931 1.2511 1.5825 105.4 SAT VAP 0.0059 460.2 1.6918 1.3775 1.7212 102.0 157.76

155 0.0068 462.3 1.6998 1.1919 1.5208 107.9 — — — — — — 155160 0.0071 468.0 1.7131 1.1072 1.4323 112.6 0.0060 463.1 1.6987 1.2898 1.6284 104.8 160165 0.0075 473.4 1.7255 1.0539 1.3758 116.7 0.0064 469.2 1.7128 1.1683 1.5000 110.1 165170 0.0078 478.6 1.7372 1.0180 1.3363 120.3 0.0067 474.9 1.7256 1.0973 1.4241 114.5 170175 0.0080 483.6 1.7485 0.9928 1.3071 123.6 0.0070 480.3 1.7376 1.0512 1.3734 118.5 175180 0.0083 488.5 1.7594 0.9748 1.2846 126.7 0.0073 485.4 1.7491 1.0197 1.3372 122.0 180185 0.0085 493.4 1.7700 0.9618 1.2666 129.6 0.0075 490.5 1.7602 0.9976 1.3099 125.2 185190 0.0088 498.2 1.7804 0.9526 1.2519 132.3 0.0078 495.4 1.7709 0.9817 1.2885 128.3 190195 0.0090 502.9 1.7906 0.9460 1.2395 134.9 0.0080 500.3 1.7814 0.9703 1.2711 131.1 195200 0.0093 507.6 1.8006 0.9416 1.2290 137.3 0.0082 505.1 1.7917 0.9622 1.2568 133.8 200205 0.0095 512.3 1.8105 0.9389 1.2199 139.7 0.0084 509.9 1.8017 0.9566 1.2446 136.4 205210 0.0097 517.0 1.8203 0.9374 1.2118 141.9 0.0087 514.7 1.8117 0.9529 1.2341 138.8 210215 0.0099 521.7 1.8299 0.9370 1.2046 144.1 0.0089 519.5 1.8215 0.9507 1.2249 141.2 215220 0.0101 526.4 1.8395 0.9373 1.1981 146.3 0.0091 524.2 1.8311 0.9496 1.2168 143.5 220225 0.0103 531.1 1.8489 0.9384 1.1921 148.3 0.0093 529.0 1.8407 0.9495 1.2094 145.7 225230 0.0106 535.8 1.8583 0.9399 1.1867 150.4 0.0095 533.7 1.8502 0.9502 1.2027 147.8 230235 0.0108 540.5 1.8676 0.9418 1.1816 152.3 0.0097 538.5 1.8596 0.9514 1.1966 149.9 235240 0.0110 545.2 1.8768 0.9441 1.1768 154.2 0.0099 543.2 1.8689 0.9531 1.1909 151.9 240245 0.0112 549.9 1.8860 0.9466 1.1723 156.1 0.0101 548.0 1.8782 0.9551 1.1856 153.9 245250 0.0114 554.7 1.8951 0.9493 1.1681 157.9 0.0103 552.8 1.8874 0.9574 1.1806 155.8 250255 0.0116 559.4 1.9042 0.9522 1.1641 159.7 0.0104 557.6 1.8965 0.9599 1.1760 157.7 255260 0.0118 564.2 1.9131 0.9551 1.1602 161.4 0.0106 562.4 1.9055 0.9626 1.1715 159.5 260265 0.0120 569.0 1.9221 0.9582 1.1566 163.1 0.0108 567.2 1.9145 0.9655 1.1673 161.3 265270 0.0121 573.8 1.9310 0.9613 1.1531 164.7 0.0110 572.0 1.9235 0.9684 1.1632 163.0 270275 0.0123 578.6 1.9398 0.9644 1.1497 166.4 0.0112 576.9 1.9324 0.9714 1.1594 164.7 275280 0.0125 583.4 1.9485 0.9675 1.1464 167.9 0.0114 581.7 1.9412 0.9744 1.1557 166.4 280285 0.0127 588.3 1.9573 0.9706 1.1433 169.5 0.0115 586.6 1.9500 0.9774 1.1521 168.0 285290 0.0129 593.1 1.9659 0.9737 1.1403 171.0 0.0117 591.5 1.9587 0.9804 1.1487 169.6 290295 0.0131 598.0 1.9746 0.9768 1.1373 172.5 0.0119 596.4 1.9674 0.9834 1.1454 171.2 295300 0.0133 602.9 1.9831 0.9798 1.1345 174.0 0.0121 601.3 1.9760 0.9864 1.1422 172.7 300305 0.0135 607.8 1.9917 0.9827 1.1317 175.4 0.0122 606.3 1.9846 0.9893 1.1391 174.2 305310 — — — — — — 0.0124 611.2 1.9931 0.9921 1.1361 175.7 310

26

Page 29: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 2600.00 kPa (abs)

PRESSURE = 3200.00 kPa (abs)

PRESSURE = 2800.00 kPa (abs)

PRESSURE = 3000.00 kPa (abs)

162.54 0.0010 382.3 1.5107 1.6127 1.9425 177.4 SAT LIQ 0.0011 389.0 1.5255 1.7856 2.1163 155.5 167.04162.54 0.0052 460.4 1.6898 1.5591 1.9206 98.5 SAT VAP 0.0046 460.0 1.6866 1.8410 2.2295 95.0 167.04

165 0.0054 464.0 1.6981 1.4051 1.7557 102.0 — — — — — — 165170 0.0058 470.5 1.7129 1.2341 1.5732 107.9 0.0049 464.9 1.6978 1.5332 1.8975 99.8 170175 0.0061 476.4 1.7262 1.1421 1.4742 112.7 0.0053 471.9 1.7136 1.3013 1.6481 106.1 175180 0.0064 482.0 1.7385 1.0847 1.4110 116.9 0.0056 478.1 1.7273 1.1862 1.5237 111.2 180185 0.0066 487.3 1.7502 1.0466 1.3672 120.6 0.0059 483.9 1.7399 1.1173 1.4475 115.6 185190 0.0069 492.5 1.7614 1.0200 1.3348 124.0 0.0061 489.3 1.7518 1.0724 1.3961 119.5 190195 0.0071 497.5 1.7723 1.0012 1.3098 127.2 0.0063 494.6 1.7631 1.0416 1.3587 123.0 195200 0.0073 502.5 1.7828 0.9876 1.2899 130.1 0.0066 499.7 1.7741 1.0199 1.3302 126.3 200205 0.0076 507.4 1.7932 0.9780 1.2735 132.9 0.0068 504.8 1.7847 1.0044 1.3077 129.4 205210 0.0078 512.3 1.8033 0.9712 1.2597 135.6 0.0070 509.8 1.7951 0.9933 1.2893 132.2 210215 0.0080 517.1 1.8133 0.9667 1.2479 138.1 0.0072 514.7 1.8053 0.9855 1.2739 135.0 215220 0.0082 522.0 1.8231 0.9638 1.2376 140.6 0.0074 519.7 1.8153 0.9801 1.2608 137.6 220225 0.0084 526.8 1.8328 0.9622 1.2284 143.0 0.0076 524.6 1.8251 0.9766 1.2495 140.1 225230 0.0086 531.6 1.8424 0.9616 1.2203 145.2 0.0078 529.4 1.8349 0.9745 1.2395 142.6 230235 0.0088 536.4 1.8519 0.9619 1.2129 147.4 0.0080 534.3 1.8445 0.9736 1.2305 144.9 235240 0.0089 541.2 1.8614 0.9628 1.2061 149.6 0.0081 539.2 1.8541 0.9735 1.2224 147.2 240245 0.0091 546.0 1.8707 0.9642 1.1998 151.7 0.0083 544.0 1.8635 0.9741 1.2150 149.4 245250 0.0093 550.9 1.8800 0.9660 1.1940 153.7 0.0085 548.9 1.8729 0.9753 1.2082 151.5 250255 0.0095 555.7 1.8892 0.9682 1.1885 155.6 0.0087 553.8 1.8821 0.9769 1.2018 153.6 255260 0.0097 560.5 1.8983 0.9705 1.1834 157.6 0.0088 558.7 1.8914 0.9789 1.1959 155.6 260265 0.0098 565.4 1.9074 0.9731 1.1785 159.4 0.0090 563.6 1.9005 0.9811 1.1903 157.5 265270 0.0100 570.3 1.9164 0.9758 1.1739 161.3 0.0092 568.5 1.9096 0.9835 1.1851 159.4 270275 0.0102 575.1 1.9253 0.9786 1.1695 163.0 0.0093 573.4 1.9186 0.9860 1.1801 161.3 275280 0.0104 580.0 1.9342 0.9814 1.1653 164.8 0.0095 578.3 1.9276 0.9887 1.1753 163.1 280285 0.0105 585.0 1.9431 0.9843 1.1613 166.5 0.0097 583.3 1.9365 0.9914 1.1708 164.9 285290 0.0107 589.9 1.9519 0.9872 1.1574 168.2 0.0098 588.3 1.9453 0.9942 1.1665 166.6 290295 0.0109 594.8 1.9606 0.9901 1.1537 169.8 0.0100 593.2 1.9541 0.9970 1.1623 168.3 295300 0.0110 599.8 1.9693 0.9930 1.1501 171.4 0.0101 598.2 1.9629 0.9998 1.1583 170.0 300305 0.0112 604.8 1.9779 0.9959 1.1467 172.9 0.0103 603.2 1.9716 1.0026 1.1545 171.6 305310 0.0114 609.8 1.9865 0.9987 1.1433 174.5 0.0105 608.3 1.9802 1.0054 1.1508 173.2 310315 0.0115 614.8 1.9951 1.0015 1.1401 176.0 0.0106 613.3 1.9888 1.0081 1.1472 174.8 315320 — — — — — — 0.0108 618.3 1.9974 1.0108 1.1437 176.3 320

171.27 0.0011 395.8 1.5402 2.0683 2.4027 133.7 SAT LIQ 0.0012 402.7 1.5552 2.6247 2.9724 111.8 175.26171.27 0.0041 458.8 1.6821 2.3286 2.7611 91.4 SAT VAP 0.0035 456.7 1.6755 3.3304 3.8424 88.1 175.26

175 0.0045 466.0 1.6982 1.6603 2.0379 98.3 — — — — — — 175180 0.0048 473.5 1.7148 1.3641 1.7184 104.9 0.0041 467.4 1.6994 1.7630 2.1509 97.5 180185 0.0051 479.9 1.7289 1.2267 1.5693 110.1 0.0045 475.2 1.7166 1.4165 1.7769 104.2 185190 0.0054 485.8 1.7417 1.1473 1.4812 114.7 0.0048 481.9 1.7310 1.2614 1.6081 109.6 190195 0.0057 491.4 1.7538 1.0963 1.4226 118.7 0.0050 487.9 1.7440 1.1734 1.5103 114.1 195200 0.0059 496.8 1.7652 1.0618 1.3807 122.3 0.0053 493.7 1.7562 1.1176 1.4460 118.2 200205 0.0061 502.1 1.7762 1.0376 1.3490 125.7 0.0055 499.1 1.7677 1.0800 1.4002 121.9 205210 0.0063 507.2 1.7869 1.0203 1.3241 128.8 0.0057 504.5 1.7788 1.0538 1.3659 125.3 210215 0.0065 512.3 1.7974 1.0080 1.3040 131.8 0.0059 509.7 1.7896 1.0351 1.3390 128.5 215220 0.0067 517.3 1.8076 0.9992 1.2872 134.6 0.0061 514.8 1.8000 1.0218 1.3173 131.5 220225 0.0069 522.3 1.8177 0.9931 1.2729 137.3 0.0063 519.9 1.8103 1.0122 1.2993 134.3 225230 0.0071 527.2 1.8276 0.9890 1.2606 139.8 0.0065 525.0 1.8204 1.0056 1.2840 137.1 230235 0.0073 532.2 1.8373 0.9865 1.2497 142.3 0.0066 530.0 1.8303 1.0011 1.2707 139.7 235240 0.0074 537.1 1.8470 0.9852 1.2400 144.7 0.0068 535.0 1.8401 0.9982 1.2591 142.2 240245 0.0076 542.0 1.8565 0.9849 1.2313 147.0 0.0070 540.0 1.8498 0.9966 1.2487 144.6 245250 0.0078 546.9 1.8660 0.9853 1.2233 149.2 0.0072 544.9 1.8593 0.9960 1.2394 147.0 250255 0.0079 551.9 1.8754 0.9862 1.2159 151.4 0.0073 549.9 1.8688 0.9962 1.2309 149.2 255260 0.0081 556.8 1.8847 0.9877 1.2091 153.5 0.0075 554.9 1.8782 0.9970 1.2230 151.4 260265 0.0083 561.7 1.8939 0.9894 1.2027 155.6 0.0076 559.9 1.8875 0.9982 1.2158 153.6 265270 0.0084 566.7 1.9030 0.9915 1.1967 157.6 0.0078 564.9 1.8967 0.9999 1.2090 155.7 270275 0.0086 571.7 1.9121 0.9938 1.1911 159.5 0.0079 569.9 1.9059 1.0018 1.2026 157.7 275280 0.0088 576.6 1.9212 0.9962 1.1858 161.4 0.0081 574.9 1.9150 1.0040 1.1966 159.7 280285 0.0089 581.6 1.9302 0.9988 1.1807 163.3 0.0083 579.9 1.9241 1.0063 1.1909 161.6 285290 0.0091 586.6 1.9391 1.0014 1.1758 165.1 0.0084 585.0 1.9330 1.0087 1.1855 163.5 290295 0.0092 591.6 1.9479 1.0040 1.1712 166.8 0.0085 590.0 1.9420 1.0112 1.1804 165.3 295300 0.0094 596.7 1.9567 1.0067 1.1668 168.6 0.0087 595.1 1.9508 1.0138 1.1755 167.1 300305 0.0095 601.7 1.9655 1.0094 1.1625 170.3 0.0088 600.2 1.9597 1.0163 1.1708 168.8 305310 0.0097 606.8 1.9742 1.0121 1.1584 171.9 0.0090 605.2 1.9684 1.0189 1.1663 170.6 310315 0.0098 611.8 1.9829 1.0148 1.1545 173.5 0.0091 610.3 1.9771 1.0215 1.1620 172.2 315320 0.0100 616.9 1.9915 1.0174 1.1507 175.1 0.0093 615.5 1.9858 1.0241 1.1578 173.9 320325 0.0101 622.0 2.0000 1.0200 1.1470 176.6 0.0094 620.6 1.9944 1.0266 1.1538 175.4 325330 — — — — — — 0.0095 625.7 2.0029 1.0290 1.1500 177.0 330

27

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TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

PRESSURE = 3600.00 kPa (abs)PRESSURE = 3400.00 kPa (abs)

179.02 0.0013 410.3 1.5715 4.2148 4.6140 90.7 SAT LIQ 0.0015 420.3 1.5930 20.2983 21.0987 73.2 182.54179.02 0.0030 452.7 1.6652 6.1872 6.8732 85.1 SAT VAP 0.0024 443.9 1.6448 30.1588 31.5405 81.4 182.54

180 0.0032 457.2 1.6753 3.6637 4.1880 88.1 — — — — — — 180185 0.0038 469.2 1.7016 1.8191 2.2123 97.6 0.0031 459.8 1.6797 3.2361 3.7187 90.1 185190 0.0042 477.2 1.7190 1.4521 1.8167 104.1 0.0036 471.4 1.7048 1.8229 2.2160 98.5 190195 0.0045 484.0 1.7337 1.2875 1.6373 109.4 0.0039 479.5 1.7222 1.4688 1.8353 104.6 195200 0.0047 490.2 1.7468 1.1943 1.5334 114.0 0.0042 486.4 1.7368 1.3040 1.6556 109.7 200205 0.0050 496.0 1.7590 1.1354 1.4652 118.0 0.0045 492.7 1.7500 1.2096 1.5498 114.2 205210 0.0052 501.6 1.7706 1.0958 1.4167 121.7 0.0047 498.5 1.7623 1.1495 1.4798 118.2 210215 0.0054 507.0 1.7817 1.0682 1.3804 125.2 0.0049 504.2 1.7739 1.1090 1.4299 121.9 215220 0.0056 512.3 1.7925 1.0486 1.3520 128.4 0.0051 509.7 1.7850 1.0807 1.3923 125.3 220225 0.0058 517.5 1.8030 1.0345 1.3290 131.4 0.0053 515.0 1.7958 1.0606 1.3628 128.5 225230 0.0059 522.6 1.8133 1.0245 1.3099 134.3 0.0054 520.3 1.8063 1.0462 1.3390 131.5 230235 0.0061 527.8 1.8234 1.0174 1.2938 137.0 0.0056 525.5 1.8166 1.0358 1.3192 134.4 235240 0.0063 532.8 1.8333 1.0125 1.2798 139.7 0.0058 530.6 1.8267 1.0285 1.3023 137.2 240245 0.0064 537.9 1.8431 1.0094 1.2675 142.2 0.0059 535.8 1.8367 1.0235 1.2878 139.8 245250 0.0066 542.9 1.8528 1.0076 1.2566 144.7 0.0061 540.9 1.8465 1.0202 1.2750 142.4 250255 0.0068 548.0 1.8624 1.0068 1.2467 147.0 0.0063 546.0 1.8562 1.0182 1.2635 144.9 255260 0.0069 553.0 1.8719 1.0068 1.2377 149.3 0.0064 551.1 1.8658 1.0173 1.2532 147.2 260265 0.0071 558.0 1.8813 1.0075 1.2294 151.6 0.0066 556.1 1.8753 1.0172 1.2438 149.6 265270 0.0072 563.1 1.8906 1.0086 1.2218 153.7 0.0067 561.2 1.8847 1.0178 1.2351 151.8 270275 0.0074 568.1 1.8999 1.0101 1.2146 155.8 0.0069 566.3 1.8940 1.0188 1.2271 154.0 275280 0.0075 573.2 1.9090 1.0120 1.2079 157.9 0.0070 571.4 1.9033 1.0202 1.2196 156.1 280285 0.0077 578.2 1.9182 1.0140 1.2016 159.9 0.0071 576.5 1.9124 1.0219 1.2126 158.2 285290 0.0078 583.3 1.9272 1.0162 1.1956 161.8 0.0073 581.6 1.9216 1.0239 1.2060 160.2 290295 0.0080 588.4 1.9362 1.0185 1.1899 163.7 0.0074 586.8 1.9306 1.0260 1.1997 162.2 295300 0.0081 593.5 1.9451 1.0209 1.1845 165.6 0.0076 591.9 1.9396 1.0282 1.1938 164.1 300305 0.0082 598.6 1.9540 1.0234 1.1793 167.4 0.0077 597.0 1.9486 1.0305 1.1881 165.9 305310 0.0084 603.7 1.9628 1.0258 1.1744 169.2 0.0078 602.2 1.9574 1.0328 1.1827 167.8 310315 0.0085 608.9 1.9716 1.0283 1.1697 170.9 0.0080 607.4 1.9663 1.0352 1.1775 169.6 315320 0.0086 614.0 1.9803 1.0308 1.1651 172.6 0.0081 612.6 1.9751 1.0376 1.1726 171.3 320325 0.0088 619.2 1.9890 1.0333 1.1608 174.2 0.0082 617.7 1.9838 1.0400 1.1679 173.0 325330 0.0089 624.3 1.9976 1.0357 1.1566 175.8 0.0083 623.0 1.9924 1.0423 1.1633 174.6 330335 — — — — — — 0.0085 628.2 2.0011 1.0446 1.1589 176.3 335

28

Page 31: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

TEMP TEMP°C V H S Cp Cp/Cv vs V H S Cp Cp/Cv vs °C

Table 2 (continued)HCFC-123 Superheated Vapor�Constant Pressure Tables

V = Volume in m3/kg H = Enthalpy in kJ/kg S = Entropy in kJ/(kg)(K) vs = Velocity of Sound in m/secCp = Heat Capacity at Constant Pressure in kJ/(kg)(°C) Cp/Cv = Heat Capacity Ratio (Dimensionless)

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29

Page 32: Thermodynamic Properties of HCFC-123, SI units · Thermodynamic Properties of HCFC-123 Refrigerant (2,2 dichloro-1,1,1-trifluoroethane) SI Units New tables of the thermodynamic properties

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